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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62373 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
AST & Science
Mission
Spacecraft
Bus & Motor
BW3 LVA, Unknown motor
Mass
150 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.0 m
Radar Cross Section
1.963 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SPACEMOBILE-SSR05 DEB
1 62373U 24163K 25241.20930032 .00011482 00000-0 45450-3 0 9997
2 62373 52.9768 205.5890 0007052 328.3830 31.6742 15.25888289 53423Epoch: 2025-08-29T05:01Z
TLE epoch observation values (Epoch: 2025-08-29T05:01:23.547Z)
Latitude
-0.00003°
Longitude
152.57963°
Altitude
484.878 km
Speed
7.626 km/s
True Right ascension
13h 42m 21s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.247 km
Perigee altitude
483.563 km
Semi-major axis
6,866.542 km
Eccentricity
0.00071
Inclination
52.9768°
RAAN
205.589°
Arg. of periapsis
328.383°
True anomaly
31.71666°
Mean anomaly
31.6742°
Eccentric anomaly
31.69543°
Mean motion
3.81449 °/min
Orbital period
94.38 mins
BSTAR
0.0004545
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-08-30 00:03:09.564Z | 210.933° SW | 2025-08-30 00:06:09.564Z | 142.973° SSE | 38.583° | 2025-08-30 00:09:09.564Z | 61.804° ENE |
| 4 mins | 2025-08-30 01:43:09.564Z | 297.48° NW | 2025-08-30 01:45:09.564Z | 346.751° N | 22.248° | 2025-08-30 01:47:09.564Z | 23.965° NE |
| 5 mins | 2025-08-30 06:40:09.564Z | 326.598° NNW | 2025-08-30 06:42:09.564Z | 19.211° NNE | 37.052° | 2025-08-30 06:45:09.564Z | 107.33° ESE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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