2008 RY19

Solar System
Dynamics
Group

2007 RY₁₉

Asteroid 2007 RY₁₉ was discovered on September 13, 2007 by the NASA-founded LINEAR asteroid survey eight days before it passed about 11 million kilometers of Earth. The object is estimated at 90—210 metres.

Number of original observations: 40
Arc : 2007 09 14 - 2007 09 25
Nominal rms: 0″.47 (80 residuals)

Possible collisions in: 2024, 2033, 2036, 2060, 2075, 2076, 2080A, 2080B, 2081, 2084, 2085A, 2085B, 2087, 2089A, 2089B, 2089C

Year: 2024

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20240306	1.102334351 2.64 1.093433615	0.248384195 2.67 0.246271611	12.3627706 2.68 12.4193332	352.4570591 2.69 352.3049086	99.2988960 -2.69 99.2988960	328.0961794 2.70 49.4006976	0″.47

Impact date: 2024 03 12.693 (UT) V_impact= 14.552 km/sec Ψ_impact = 48°.51

dev/σ: Deviation from the nominal orbit parameter divided by the respective uncertainty.

V_impact: The velocity of the asteroid relative to the Earth at the moment of impact.

Ψ_impact: The impact angle is measured from the vertical axis that goes through the impact point. Thus, the impact angle is 0 degrees for a vertical impact.

rms: Root mean square for the derived impact orbit.

Year: 2033

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20330306	1.102363114 2.62 1.087325333	0.248406376 2.66 0.244773646	12.3640110 2.67 12.4602759	352.4574469 2.68 352.2359714	99.2962327 -2.68 96.6962978	328.0998447 2.68 50.2398878	0″.59

Impact date: 2033 03 12.932 (UT) V_impact= 14.364 km/sec Ψ_impact = 12°.22

Year: 2036

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20360306	1.102464883 2.58 1.114751374	0.248488342 2.62 0.251301990	12.3684348 2.63 12.3292771	352.4588109 2.63 352.2294764	99.2873321 -2.62 101.6668725	328.1127566 2.64 45.7998462	0″.48

Impact date: 2036 03 12.698 (UT) V_impact= 14.513 km/sec Ψ_impact = 41°.71

Year: 2060

Orbital elements of impact orbit for two dates (equ. J2000)


Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20600306	1.102069160 2.75 1.104309347	0.248139403 2.79 0.248742563	12.3500351 2.80 12.3392428	352.4531286 2.81 352.0525687	99.3176741 -2.81 99.8301694	328.0631201 2.82 47.5225936	0″.60

Impact date: 2060 03 12.677 (UT) V_impact= 14.420 km/sec Ψ_impact = 24°.98

Year: 2075

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20750306	1.104990387 1.47 1.101302800	0.250766399 1.48 0.250023650	12.4873463 1.48 12.4993133	352.4954978 1.48 352.0067335	99.1050848 -1.50 98.9403375	328.4246253 1.49 47.4313043	0″.53

Impact date: 2075 03 13.474 (UT) V_impact= 14.753 km/sec Ψ_impact = 72°.51

Year: 2076

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20760306	1.105026506 1.46 1.099111909	0.250786749 1.47 0.249447196	12.4886266 1.47 12.5163510	352.4959013 1.47 351.9822608	99.1007560 -1.47 98.5995998	328.4292840 1.47 48.4180393	0″.49

Impact date: 2076 03 12.724 (UT) V_impact= 14.504 km/sec Ψ_impact = 51°.77

Year: 2080

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20800306	1.105312569 1.33 1.106107983	0.251043161 1.34 0.251446961	12.5019158 1.34 12.4882401	352.4999849 1.34 351.9760345	99.0803370 -1.35 99.7693998	328.4642329 1.35 47.2686310	0″.49

Impact date: 2080 03 12.723 (UT) V_impact= 14.589 km/sec Ψ_impact = 44°.54

dev/σ

20071027

20800306

1.105389667
1.30
1.106133609

0.251103422
1.31
0.251530998

12.5052463
1.31
12.4903294

352.5010238
1.31
351.9841205

99.0735576
-1.31
99.7615569

328.4738055
1.31
47.2598894

0″.48

Impact date: 2080 03 12.731 (UT) V_impact= 14.564 km/sec Ψ_impact = 40°.15

Year: 2081

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20810306	1.105945890 1.05 1.105945890	0.251599529 1.06 0.251289206	12.5311125 1.06 12.5343787	352.5089979 1.06 351.9780710	99.0337713 -1.06 99.3895601	328.5414972 1.06 47.3652400	0″.47

Impact date: 2081 03 13.004 (UT) V_impact= 14.539 km/sec Ψ_impact = 55°.31

Year: 2084

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20840306	1.106013483 1.02 1.097026369	0.251653262 1.03 0.249210865	12.5340555 1.03 12.6049167	352.5099140 1.03 351.9525985	99.0280033 -1.03 98.1887653	328.5498296 1.03 48.7531230	0″.48

Impact date: 2084 03 12.755 (UT) V_impact= 14.724 km/sec Ψ_impact = 81°.85

Year: 2085

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20850306	1.105169292 1.39 1.108954753	0.250915617 1.40 0.251878894	12.4953275 1.40 12.4777212	352.4979667 1.41 351.9269476	99.0906755 -1.41 100.3150808	328.4467129 1.41 46.5906485	0″.49

Impact date: 2085 03 12.962 (UT) V_impact= 14.660 km/sec Ψ_impact = 56°.12

dev/σ

20071027

20850306

1.105224627
1.37
1.110530871

0.250965810
1.38
0.252369220

12.4979091
1.38
12.4696446

352.4987579
1.38
351.9376083

99.0868144
-1.39
100.5963452

328.4534619
1.39
46.3112423

0″.49

Impact date: 2085 03 12.981 (UT) V_impact= 14.393 km/sec Ψ_impact = 9°.90

Year: 2087

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20870306	1.106041871 1.01 1.091470672	0.251684352 1.02 0.243348647	12.5355535 1.02 12.9177579	352.5103687 1.02 351.9217871	99.0268240 -1.02 97.8789287	328.5531605 1.02 48.9470124	0″.47

Impact date: 2087 03 13.471 (UT) V_impact= 14.402 km/sec Ψ_impact = 11°.59

Year: 2089

Orbital elements of impact orbit for two dates (equ. J2000)

	Epoch [TT]	a [AU]	e	i [deg]	Ω [deg]	ω [deg]	M [deg]	rms
dev/σ	20071027 20890306	1.104612199 1.64 1.101891283	0.250410686 1.65 0.249995145	12.4690680 1.66 12.4611244	352.4898682 1.66 351.8910592	99.1298249 -1.65 99.1086797	328.3786435 1.66 47.7453093	0″.50

Impact date: 2089 03 12.963 (UT) V_impact= 14.401 km/sec Ψ_impact = 30°.51

dev/σ

20071027

20890306

1.104847321
1.53
1.100550980

0.250624492
1.55
0.249766284

12.4802425
1.55
12.4851338

352.4933259
1.55
351.8935100

99.1133526
-1.55
98.8430121

328.4073829
1.55
47.9794099

0″.50

Impact date: 2089 03 12.959 (UT) V_impact= 14.380 km/sec Ψ_impact = 5°.35

dev/σ

20071027

20890306

1.105965123

1.102031358

0.251612952
1.04
0.250759318

12.5318478
1.05
12.5427331

352.5092213
1.05
351.9294115

99.0318643
-1.05
98.9895005

328.5439152
1.05
47.7347163

0″.47

Impact date: 2089 03 12.990 (UT) V_impact= 14.493 km/sec Ψ_impact = 23°.82

Number of original observations: 40
Arc : 2007 09 14 - 2007 09 25
Nominal rms: 0″.47 (80 residuals)

Possible collisions in: 2024, 2033, 2036, 2060, 2075, 2076, 2080A, 2080B, 2081, 2084, 2085A, 2085B, 2087, 2089A, 2089B, 2089C

Year: 2024

Year: 2033

Year: 2036

Year: 2060

Year: 2075

Year: 2076

Year: 2080

Year: 2081

Year: 2084

Year: 2085

Year: 2087

Year: 2089

External links:

2007 RY₁₉ page (NASA JPL) and Impact Risk page NEO Program (NASA JPL)
2007 RY₁₉ page and Impact Risk page at the NEO Dynamic Site (NEODyS)

Solar System Dynamics & Planetology Group, 2008. All rights reserved

Number of original observations: 40 Arc : 2007 09 14 - 2007 09 25 Nominal rms: 0″.47 (80 residuals) Possible collisions in: 2024, 2033, 2036, 2060, 2075, 2076, 2080A, 2080B, 2081, 2084, 2085A, 2085B, 2087, 2089A, 2089B, 2089C

Year: 2024

Year: 2033

Year: 2036

Year: 2060

Year: 2075

Year: 2076

Year: 2080

Year: 2081

Year: 2084

Year: 2085

Year: 2087

Year: 2089

External links:

2007 RY19 page (NASA JPL) and Impact Risk page NEO Program (NASA JPL) 2007 RY19 page and Impact Risk page at the NEO Dynamic Site (NEODyS)

Solar System Dynamics & Planetology Group, 2008. All rights reserved

Number of original observations: 40
Arc : 2007 09 14 - 2007 09 25
Nominal rms: 0″.47 (80 residuals)

Possible collisions in: 2024, 2033, 2036, 2060, 2075, 2076, 2080A, 2080B, 2081, 2084, 2085A, 2085B, 2087, 2089A, 2089B, 2089C

2007 RY₁₉ page (NASA JPL) and Impact Risk page NEO Program (NASA JPL)
2007 RY₁₉ page and Impact Risk page at the NEO Dynamic Site (NEODyS)