SPACEMOBILE-SSR03 DEB, 62371

Orbit data source: Space-Track

SPACEMOBILE-SSR03 DEB, 62371 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/62371?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

62371, 2024-163H

Orbit

LEO

Last TLE update

5 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 (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 5 hours ago

0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   25222.59824840  .00012917  00000-0  47488-3 0  9992
2 62371  52.9739 289.5235 0008745 253.5989 106.4048 15.28221449 44206

Epoch: 2025-08-10T14:21Z

TLE epoch observation values (Epoch: 2025-08-10T14:21:28.661Z)

Latitude

0.00002°

Longitude

114.83679°

Altitude

483.707 km

Speed

7.624 km/s

True Right ascension

19h 18m 05s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

10.71753°

Longitude

-74.3787°

Altitude

480.996 km

Speed

7.627 km/s

Apparent Right ascension

03h 36m 38s

Apparent Declination

-27° 57' 48"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

10:05:16

Azimuth

251.747° W

Elevation

-22.661°

Doppler factor

Orbital elements

Apogee altitude

487.414 km

Perigee altitude

475.417 km

Semi-major axis

6,859.552 km

Eccentricity

0.00087

Inclination

52.9739°

RAAN

289.5235°

Arg. of periapsis

253.5989°

True anomaly

106.5009°

Mean anomaly

106.4048°

Eccentric anomaly

106.45285°

Mean motion

3.82032 °/min

Orbital period

94.23 mins

BSTAR

0.00047488

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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-SSR04 DEB, 62372

SPACEMOBILE-SSR05 DEB, 62373

SPACEMOBILE-SSR03 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 06:12:34.911Z	171.696° S	2025-08-11 06:14:34.911Z	134.254° SE	19.36°	2025-08-11 06:17:34.911Z	80.182° E
5 mins	2025-08-11 07:50:34.911Z	260.358° W	2025-08-11 07:52:34.911Z	323.549° NNW	36.616°	2025-08-11 07:55:34.911Z	37.874° NE
4 mins	2025-08-11 12:48:34.911Z	353.818° N	2025-08-11 12:49:34.911Z	17.748° NNE	22.842°	2025-08-11 12:52:34.911Z	79.926° E
6 mins	2025-08-11 14:25:34.911Z	295.526° NW	2025-08-11 14:28:34.911Z	197.766° SSW	36.566°	2025-08-11 14:31:34.911Z	148.753° 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-SSR03 DEB, 62371 on other resources

View SPACEMOBILE-SSR03 DEB, 62371 on Heavens-Above

View SPACEMOBILE-SSR03 DEB, 62371 on Keep Track

View SPACEMOBILE-SSR03 DEB, 62371 on Celestrak

View SPACEMOBILE-SSR03 DEB, 62371 on Gunter's Space Page

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