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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62372 intel report (Beta)
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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, 3.8 m
Radar Cross Section
1.963 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 SPACEMOBILE-SSR04 DEB
1 62372U 24163J 26093.62552916 .00029170 00000-0 78107-3 0 9997
2 62372 52.9843 263.2543 0004336 294.0571 65.9977 15.37801499 83474Epoch: 2026-04-03T15:00Z
TLE epoch observation values (Epoch: 2026-04-03T15:00:45.719Z)
Latitude
-0°
Longitude
-153.89317°
Altitude
452.292 km
Speed
7.643 km/s
True Right ascension
17h 33m 01s
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
03:39:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.86 km
Perigee altitude
449.936 km
Semi-major axis
6,831.035 km
Eccentricity
0.00043
Inclination
52.9843°
RAAN
263.2543°
Arg. of periapsis
294.0571°
True anomaly
66.0431°
Mean anomaly
65.9977°
Eccentric anomaly
66.0204°
Mean motion
3.84427 °/min
Orbital period
93.65 mins
BSTAR
0.00078107
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SPACEMOBILE-SSR04 DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-04 13:01:33.740Z | 161.168° S | 2026-04-04 13:02:33.740Z | 136.252° SSE | 21.754° | 2026-04-04 13:05:33.740Z | 76.669° E |
| 4 mins | 2026-04-04 14:38:33.740Z | 276.265° WNW | 2026-04-04 14:39:33.740Z | 305.819° NW | 30.933° | 2026-04-04 14:42:33.740Z | 31.815° NE |
| 4 mins | 2026-04-04 19:33:33.740Z | 343.573° N | 2026-04-04 19:35:33.740Z | 33.19° NE | 23.639° | 2026-04-04 19:37:33.740Z | 77.706° E |
| 4 mins | 2026-04-04 21:11:33.740Z | 276.834° WNW | 2026-04-04 21:12:33.740Z | 243.958° WSW | 33.17° | 2026-04-04 21:15:33.740Z | 157.892° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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