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: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-002
1 61048U 24163D 26125.53211141 .00003415 00000-0 16694-3 0 9991
2 61048 52.9749 145.2728 0007665 7.3309 352.7796 15.20916462 91276Epoch: 2026-05-05T12:46Z
TLE epoch observation values (Epoch: 2026-05-05T12:46:14.425Z)
Latitude
-0.00004°
Longitude
90.30706°
Altitude
498.719 km
Speed
7.619 km/s
True Right ascension
09h 41m 05s
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
12:02:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.635 km
Perigee altitude
498.085 km
Semi-major axis
6,881.497 km
Eccentricity
0.00077
Inclination
52.9749°
RAAN
145.2728°
Arg. of periapsis
7.3309°
True anomaly
352.76855°
Mean anomaly
352.7796°
Eccentric anomaly
352.77408°
Mean motion
3.80206 °/min
Orbital period
94.69 mins
BSTAR
0.00016694
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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 | 2026-05-06 04:44:57.704Z | 256.527° W | 2026-05-06 04:47:57.704Z | 321.164° NNW | 34.168° | 2026-05-06 04:50:57.704Z | 35.076° NE |
| 5 mins | 2026-05-06 09:44:57.704Z | 342.518° N | 2026-05-06 09:46:57.704Z | 31.438° NE | 25.963° | 2026-05-06 09:49:57.704Z | 88.312° E |
| 6 mins | 2026-05-06 11:22:57.704Z | 290.489° WNW | 2026-05-06 11:25:57.704Z | 204.903° SW | 33.065° | 2026-05-06 11:28:57.704Z | 155.05° SSE |
| 4 mins | 2026-05-07 02:47:57.704Z | 159.65° S | 2026-05-07 02:48:57.704Z | 135.333° SSE | 22.897° | 2026-05-07 02:51:57.704Z | 77.269° E |
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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