SPACEMOBILE-SSR02 DEB, 62370
Orbit data source: Space-Track
SPACEMOBILE-SSR02 DEB, 62370 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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62370 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: 19 hours ago
TLE from 19 hours ago
0 SPACEMOBILE-SSR02 DEB
1 62370U 24163G 26305.42189590 .00029531 00000-0 56014-3 0 9997
2 62370 52.9412 329.5152 0004252 289.6300 70.4247 15.48088297119581Epoch: 2026-11-01T10:07Z
TLE epoch observation values (Epoch: 2026-11-01T10:07:31.805Z)
Latitude
0°
Longitude
136.91918°
Altitude
422.234 km
Speed
7.66 km/s
True Right ascension
21h 58m 03s
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
01:21:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.504 km
Perigee altitude
419.721 km
Semi-major axis
6,800.75 km
Eccentricity
0.00043
Inclination
52.9412°
RAAN
329.5152°
Arg. of periapsis
289.63°
True anomaly
70.47062°
Mean anomaly
70.4247°
Eccentric anomaly
70.44766°
Mean motion
3.86997 °/min
Orbital period
93.02 mins
BSTAR
0.00056014
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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-SSR02 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-02 11:26:20.693Z | 298.864° NW | 2026-11-02 11:28:20.693Z | 190.797° SSW | 63.393° | 2026-11-02 11:31:20.693Z | 139.854° SSE |
| 5 mins | 2026-11-03 04:09:20.693Z | 229.941° WSW | 2026-11-03 04:11:20.693Z | 43.49° NE | 83° | 2026-11-03 04:14:20.693Z | 50.128° ENE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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