SPACEMOBILE-SSR02 DEB, 62370

Orbit data source: Space-Track

SPACEMOBILE-SSR02 DEB, 62370 is space debris in LEO originally from a launch on Thu, 12 Sep 2024 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier	62370, 2024-163G
Orbit	LEO
Last TLE update	8 hours ago
Origin	AST & Science (US)
Manufacturer	AST & Science
Mission	Spacecraft
Bus & Motor	BW3 LVA, Unknown motor
Mass	150 kg wet, 150 kg dry
Launch date (UTC)	2024-09-12 (6 months ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 2 m
Radar Cross Section	1.963 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 8 hours ago

0 SPACEMOBILE-SSR02 DEB
1 62370U 24163G   25070.85457444  .00016787  00000-0  69515-3 0  9997
2 62370  52.9448 272.1305 0012158 160.3875 199.7590 15.23996155 27453

Epoch: 2025-03-11T20:30Z

Definitive object data (Epoch: 2025-03-11T20:30:35.231Z)

Latitude	-0.00004°
Longitude	154.73213°
Altitude	502.54 km
Speed	7.61 km/s
True Right ascension	18h 08m 31s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	36.83929°
Longitude	-61.12729°
Altitude	489.446 km
Speed	7.629 km/s
Apparent Right ascension	00h 46m 07s
Apparent Declination	0° 12' 49"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	09:17:08
Azimuth	296.59° NW
Elevation	-27.854°
Doppler factor	1

Orbital elements

Apogee altitude	502.447 km
Perigee altitude	485.737 km
Semi-major axis	6,872.229 km
Eccentricity	0.0012158
Inclination	52.9448°
RAAN	272.1305°
Arg. of periapsis	160.3875°
True anomaly	199.71197°
Mean anomaly	199.759°
Eccentric anomaly	199.73548°
Mean motion	3.80975 °/min
BSTAR	0.00069515
Orbital period	94.49 mins

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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)

SPACEMOBILE-003, 61045

SPACEMOBILE-005, 61046

SPACEMOBILE-001, 61047

SPACEMOBILE-002, 61048

SPACEMOBILE-004, 61049

SPACEMOBILE-SSR01 DEB, 62369

SPACEMOBILE-SSR03 DEB, 62371

SPACEMOBILE-SSR04 DEB, 62372

SPACEMOBILE-SSR05 DEB, 62373

SPACEMOBILE-SSR02 DEB Visibility forecast

Observer location: undefined°, undefined

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
7 mins	2025-03-12 15:33:13.676Z	206.856° SW	2025-03-12 15:36:13.676Z	155.37° SSE	34.356°	2025-03-12 15:40:13.676Z	61.789° ENE
5 mins	2025-03-12 17:13:13.676Z	287.45° WNW	2025-03-12 17:15:13.676Z	335.928° NNW	24.893°	2025-03-12 17:18:13.676Z	31.297° NE
5 mins	2025-03-12 22:11:13.676Z	332.128° NNW	2025-03-12 22:13:13.676Z	33.266° NE	34.864°	2025-03-12 22:16:13.676Z	104.331° ESE
4 mins	2025-03-12 23:50:13.676Z	257.003° W	2025-03-12 23:51:13.676Z	233.694° WSW	21.05°	2025-03-12 23:54:13.676Z	178.188° S

Authenticating...

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Check out SPACEMOBILE-SSR02 DEB, 62370 on other resources

View SPACEMOBILE-SSR02 DEB, 62370 on Heavens-Above

View SPACEMOBILE-SSR02 DEB, 62370 on Keep Track

View SPACEMOBILE-SSR02 DEB, 62370 on Celestrak

View SPACEMOBILE-SSR02 DEB, 62370 on Gunter's Space Page

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