SPACEMOBILE-SSR04 DEB, 62372

Orbit data source: Space-Track

SPACEMOBILE-SSR04 DEB, 62372 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/62372?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62372, 2024-163J

Orbit

LEO

Last TLE update

1 week 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 (11 months ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.0 m

Radar Cross Section

1.963 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 week ago

0 SPACEMOBILE-SSR04 DEB
1 62372U 24163J   25215.65384061  .00008270  00000-0  31131-3 0  9993
2 62372  52.9889 320.5931 0004965 260.5344  99.5092 15.27973077 46219

Epoch: 2025-08-03T15:41Z

TLE epoch observation values (Epoch: 2025-08-03T15:41:31.828Z)

Latitude

-0.00007°

Longitude

132.73787°

Altitude

483.317 km

Speed

7.625 km/s

True Right ascension

21h 22m 22s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

8.79322°

Longitude

106.24075°

Altitude

481.561 km

Speed

7.627 km/s

Apparent Right ascension

20h 14m 45s

Apparent Declination

-14° 48' 52"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

09:08:06

Azimuth

28.692° NE

Elevation

-62.32°

Doppler factor

Orbital elements

Apogee altitude

485.562 km

Perigee altitude

478.75 km

Semi-major axis

6,860.293 km

Eccentricity

0.0005

Inclination

52.9889°

RAAN

320.5931°

Arg. of periapsis

260.5344°

True anomaly

99.56531°

Mean anomaly

99.5092°

Eccentric anomaly

99.53725°

Mean motion

3.8197 °/min

Orbital period

94.25 mins

BSTAR

0.00031131

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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-SSR02 DEB, 62370

SPACEMOBILE-SSR03 DEB, 62371

SPACEMOBILE-SSR05 DEB, 62373

SPACEMOBILE-SSR04 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.
5 mins	2025-08-11 07:33:34.925Z	247.632° W	2025-08-11 07:35:34.925Z	296.975° NW	40.195°	2025-08-11 07:38:34.925Z	40.821° NE
4 mins	2025-08-11 12:31:34.925Z	350.497° N	2025-08-11 12:33:34.925Z	35.414° NE	20.027°	2025-08-11 12:35:34.925Z	71.564° E
5 mins	2025-08-11 14:09:34.925Z	299.151° NW	2025-08-11 14:11:34.925Z	212.302° SW	42.739°	2025-08-11 14:14:34.925Z	141.025° SSE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Authenticating...

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Check out SPACEMOBILE-SSR04 DEB, 62372 on other resources

View SPACEMOBILE-SSR04 DEB, 62372 on Heavens-Above

View SPACEMOBILE-SSR04 DEB, 62372 on Keep Track

View SPACEMOBILE-SSR04 DEB, 62372 on Celestrak

View SPACEMOBILE-SSR04 DEB, 62372 on Gunter's Space Page

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