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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Iframe URL

https://www.satcat.com/sats-embedded/62370?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

62370, 2024-163G

Orbit

LEO

Last TLE update

11 hours ago

Origin

AST SpaceMoblie (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 (8 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 11 hours ago

0 SPACEMOBILE-SSR02 DEB
1 62370U 24163G   25133.94345387  .00011027  00000-0  42483-3 0  9996
2 62370  52.9485 339.7227 0009802  14.0253 346.1014 15.26819275 37083

Epoch: 2025-05-13T22:38Z

Definitive object data (Epoch: 2025-05-13T22:38:34.414Z)

Latitude

-0.00001°

Longitude

128.14437°

Altitude

479.673 km

Speed

7.631 km/s

True Right ascension

22h 38m 53s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

53.05575°

Longitude

-147.34035°

Altitude

489.765 km

Speed

7.628 km/s

Apparent Right ascension

05h 29m 32s

Apparent Declination

9° 09' 12"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

18:30:30

Azimuth

19.497° NNE

Elevation

-38.939°

Doppler factor

Orbital elements

Apogee altitude

492.346 km

Perigee altitude

478.89 km

Semi-major axis

6,863.755 km

Eccentricity

0.0009802

Inclination

52.9485°

RAAN

339.7227°

Arg. of periapsis

14.0253°

True anomaly

346.07439°

Mean anomaly

346.1014°

Eccentric anomaly

346.0879°

Mean motion

3.81681 °/min

BSTAR

0.00042483

Orbital period

94.32 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.
6 mins	2025-05-14 16:05:22.626Z	212.077° SW	2025-05-14 16:08:22.626Z	146.481° SSE	38.892°	2025-05-14 16:11:22.626Z	61.45° ENE
4 mins	2025-05-14 17:45:22.626Z	298.244° NW	2025-05-14 17:46:22.626Z	320.583° NNW	21.75°	2025-05-14 17:49:22.626Z	24.165° NE
5 mins	2025-05-14 22:42:22.626Z	328.103° NNW	2025-05-14 22:44:22.626Z	33.269° NE	37.905°	2025-05-14 22:47:22.626Z	109.588° ESE

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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