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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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: 7 hours ago
TLE from 7 hours ago
0 SPACEMOBILE-002
1 61048U 24163D 26305.95003535 .00009870 00000-0 46385-3 0 9994
2 61048 52.9794 35.8919 0006974 154.5518 205.5821 15.20202977118724Epoch: 2026-11-01T22:48Z
TLE epoch observation values (Epoch: 2026-11-01T22:48:03.054Z)
Latitude
0.00002°
Longitude
12.64513°
Altitude
510.435 km
Speed
7.608 km/s
True Right ascension
02h 23m 34s
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
01:22:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.313 km
Perigee altitude
500.712 km
Semi-major axis
6,883.649 km
Eccentricity
0.0007
Inclination
52.9794°
RAAN
35.8919°
Arg. of periapsis
154.5518°
True anomaly
205.54762°
Mean anomaly
205.5821°
Eccentric anomaly
205.56486°
Mean motion
3.80028 °/min
Orbital period
94.73 mins
BSTAR
0.00046385
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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 | 2026-11-02 08:26:00.062Z | 198.47° SSW | 2026-11-02 08:29:00.062Z | 121.175° SE | 40.211° | 2026-11-02 08:32:00.062Z | 65.174° ENE |
| 5 mins | 2026-11-02 10:05:00.062Z | 277.828° WNW | 2026-11-02 10:07:00.062Z | 319.228° NNW | 29.594° | 2026-11-02 10:10:00.062Z | 26.804° NE |
| 6 mins | 2026-11-02 15:04:00.062Z | 330.897° NNW | 2026-11-02 15:06:00.062Z | 17.795° NNE | 39.889° | 2026-11-02 15:10:00.062Z | 104.764° ESE |
| 5 mins | 2026-11-02 16:43:00.062Z | 270.362° WNW | 2026-11-02 16:45:00.062Z | 223.465° SW | 25.961° | 2026-11-02 16:48:00.062Z | 171.981° 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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