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: 17 hours ago
TLE from 17 hours ago
0 SPACEMOBILE-002
1 61048U 24163D 25308.59107392 .00003279 00000-0 16092-3 0 9991
2 61048 52.9710 262.2575 0010694 166.6664 193.4615 15.20892692 63584Epoch: 2025-11-04T14:11Z
TLE epoch observation values (Epoch: 2025-11-04T14:11:08.786Z)
Latitude
-0.00002°
Longitude
5.39498°
Altitude
511.179 km
Speed
7.606 km/s
True Right ascension
17h 29m 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
02:41:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.792 km
Perigee altitude
496.073 km
Semi-major axis
6,881.569 km
Eccentricity
0.00107
Inclination
52.971°
RAAN
262.2575°
Arg. of periapsis
166.6664°
True anomaly
193.43301°
Mean anomaly
193.4615°
Eccentric anomaly
193.44725°
Mean motion
3.802 °/min
Orbital period
94.69 mins
BSTAR
0.00016092
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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 | 2025-11-05 23:29:56.473Z | 223.214° SW | 2025-11-05 23:31:56.473Z | 181.299° SSW | 44.217° | 2025-11-05 23:35:56.473Z | 52.38° ENE |
| 4 mins | 2025-11-06 01:09:56.473Z | 312.83° NW | 2025-11-06 01:10:56.473Z | 334.452° NNW | 19.669° | 2025-11-06 01:13:56.473Z | 26.996° NE |
| 6 mins | 2025-11-06 06:06:56.473Z | 314.713° NW | 2025-11-06 06:09:56.473Z | 75.977° E | 43.214° | 2025-11-06 06:12:56.473Z | 123.36° SE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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