SPACEMOBILE-002, 61048
Orbit data source: Space-Track
SPACEMOBILE-002, 61048 is a payload satellite owned by AST & Science (US) in LEO that was launched on Thu, 12 Sep 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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61048 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BW3, Unknown motor
Mass
1,500 kg wet, 1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Plate, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-002
1 61048U 24163D 25289.20539066 .00004360 00000-0 20958-3 0 9992
2 61048 52.9808 351.4072 0011599 111.6512 248.5718 15.20804531 60636Epoch: 2025-10-16T04:55Z
TLE epoch observation values (Epoch: 2025-10-16T04:55:45.753Z)
Latitude
-0.00006°
Longitude
-107.50194°
Altitude
507.213 km
Speed
7.61 km/s
True Right ascension
23h 25m 37s
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
11:03:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.679 km
Perigee altitude
495.715 km
Semi-major axis
6,881.834 km
Eccentricity
0.00116
Inclination
52.9808°
RAAN
351.4072°
Arg. of periapsis
111.6512°
True anomaly
248.44814°
Mean anomaly
248.5718°
Eccentric anomaly
248.50996°
Mean motion
3.80178 °/min
Orbital period
94.69 mins
BSTAR
0.00020958
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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-002 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 06:19:40.214Z | 200.796° SSW | 2025-10-17 06:22:40.214Z | 129.89° SE | 33.355° | 2025-10-17 06:25:40.214Z | 66.023° ENE |
| 4 mins | 2025-10-17 07:59:40.214Z | 290.924° WNW | 2025-10-17 08:01:40.214Z | 345.512° N | 25.461° | 2025-10-17 08:03:40.214Z | 25.195° NE |
| 5 mins | 2025-10-17 12:57:40.214Z | 330.207° NNW | 2025-10-17 12:59:40.214Z | 18.036° NNE | 33.048° | 2025-10-17 13:02:40.214Z | 99.414° ESE |
| 4 mins | 2025-10-17 14:36:40.214Z | 268.522° W | 2025-10-17 14:38:40.214Z | 221.743° SW | 22.624° | 2025-10-17 14:40:40.214Z | 182.267° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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