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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SPACEMOBILE-002 radio frequencies
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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, 4.5 m
Radar Cross Section
1.500 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 25258.05218265 .00003180 00000-0 15804-3 0 9999
2 61048 52.9708 134.6292 0011112 28.0220 332.1370 15.20554142 55894Epoch: 2025-09-15T01:15Z
TLE epoch observation values (Epoch: 2025-09-15T01:15:08.58Z)
Latitude
-0.00006°
Longitude
121.58103°
Altitude
498.285 km
Speed
7.62 km/s
True Right ascension
08h 58m 30s
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
11:12:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.102 km
Perigee altitude
496.806 km
Semi-major axis
6,882.591 km
Eccentricity
0.00111
Inclination
52.9708°
RAAN
134.6292°
Arg. of periapsis
28.022°
True anomaly
332.07742°
Mean anomaly
332.137°
Eccentric anomaly
332.10722°
Mean motion
3.80115 °/min
Orbital period
94.71 mins
BSTAR
0.00015804
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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 | 2025-09-15 18:47:38.393Z | 236.266° WSW | 2025-09-15 18:50:38.393Z | 325.786° NNW | 44.095° | 2025-09-15 18:53:38.393Z | 46.462° ENE |
| 4 mins | 2025-09-15 23:47:38.393Z | 348.912° N | 2025-09-15 23:49:38.393Z | 30.362° NE | 19.233° | 2025-09-15 23:51:38.393Z | 66.164° ENE |
| 6 mins | 2025-09-16 01:25:38.393Z | 307.088° NW | 2025-09-16 01:28:38.393Z | 154.404° SSE | 43.268° | 2025-09-16 01:31:38.393Z | 134.262° SE |
| 4 mins | 2025-09-16 18:28:38.393Z | 242.253° WSW | 2025-09-16 18:30:38.393Z | 354.908° N | 43.2° | 2025-09-16 18:32:38.393Z | 43.255° NE |
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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