SPACEMOBILE-SSR05 DEB, 62373

Orbit data source: Space-Track

SPACEMOBILE-SSR05 DEB, 62373 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/62373?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

62373, 2024-163K

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-SSR05 DEB
1 62373U 24163K   25222.60595033  .00009086  00000-0  36566-3 0  9993
2 62373  52.9776 291.7778 0006939 255.9703 104.0522 15.25601113 50585

Epoch: 2025-08-10T14:32Z

TLE epoch observation values (Epoch: 2025-08-10T14:32:34.108Z)

Latitude

-0.00003°

Longitude

114.31077°

Altitude

491.019 km

Speed

7.62 km/s

True Right ascension

19h 27m 06s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

49.17654°

Longitude

-126.93895°

Altitude

498.609 km

Speed

7.619 km/s

Apparent Right ascension

00h 33m 52s

Apparent Declination

8° 45' 34"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

10:01:48

Azimuth

315.363° NNW

Elevation

-29.967°

Doppler factor

Orbital elements

Apogee altitude

494.032 km

Perigee altitude

484.501 km

Semi-major axis

6,867.403 km

Eccentricity

0.00069

Inclination

52.9776°

RAAN

291.7778°

Arg. of periapsis

255.9703°

True anomaly

104.12932°

Mean anomaly

104.0522°

Eccentric anomaly

104.09076°

Mean motion

3.81377 °/min

Orbital period

94.39 mins

BSTAR

0.00036566

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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-SSR04 DEB, 62372

SPACEMOBILE-SSR05 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 06:25:08.078Z	177.661° S	2025-08-11 06:28:08.078Z	117.708° SE	20.615°	2025-08-11 06:30:08.078Z	82.237° E
6 mins	2025-08-11 08:03:08.078Z	258.546° W	2025-08-11 08:06:08.078Z	348.92° N	34.022°	2025-08-11 08:09:08.078Z	39.381° NE
4 mins	2025-08-11 13:02:08.078Z	352.191° N	2025-08-11 13:03:08.078Z	16.498° NNE	24.074°	2025-08-11 13:06:08.078Z	81.562° E
5 mins	2025-08-11 14:40:08.078Z	284.525° WNW	2025-08-11 14:42:08.078Z	211.719° SW	35.508°	2025-08-11 14:45:08.078Z	152.949° 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-SSR05 DEB, 62373 on other resources

View SPACEMOBILE-SSR05 DEB, 62373 on Heavens-Above

View SPACEMOBILE-SSR05 DEB, 62373 on Keep Track

View SPACEMOBILE-SSR05 DEB, 62373 on Celestrak

View SPACEMOBILE-SSR05 DEB, 62373 on Gunter's Space Page

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