SPACEMOBILE-004, 61049
Orbit data source: Space-Track
SPACEMOBILE-004, 61049 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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61049 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: 21 hours ago
TLE from 21 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 25292.40967363 .00008279 00000-0 38422-3 0 9992
2 61049 52.9799 336.4990 0011113 127.7210 232.4793 15.20833545 61120Epoch: 2025-10-19T09:49Z
TLE epoch observation values (Epoch: 2025-10-19T09:49:55.801Z)
Latitude
-0.00005°
Longitude
160.88971°
Altitude
508.865 km
Speed
7.608 km/s
True Right ascension
22h 25m 59s
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
01:15:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.257 km
Perigee altitude
495.962 km
Semi-major axis
6,881.746 km
Eccentricity
0.00111
Inclination
52.9799°
RAAN
336.499°
Arg. of periapsis
127.721°
True anomaly
232.37838°
Mean anomaly
232.4793°
Eccentric anomaly
232.42883°
Mean motion
3.80185 °/min
Orbital period
94.69 mins
BSTAR
0.00038422
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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-004 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 | 2025-10-20 06:33:16.205Z | 263.37° W | 2025-10-20 06:36:16.205Z | 339.049° N | 31.668° | 2025-10-20 06:39:16.205Z | 36.09° NE |
| 4 mins | 2025-10-20 11:33:16.205Z | 347.534° N | 2025-10-20 11:35:16.205Z | 45.113° ENE | 26.715° | 2025-10-20 11:37:16.205Z | 85.688° E |
| 5 mins | 2025-10-20 13:11:16.205Z | 282.659° WNW | 2025-10-20 13:13:16.205Z | 230.77° WSW | 30.872° | 2025-10-20 13:16:16.205Z | 162.905° S |
| 5 mins | 2025-10-21 04:35:16.205Z | 175.147° S | 2025-10-21 04:37:16.205Z | 125.167° SE | 25.59° | 2025-10-21 04:40:16.205Z | 71.726° E |
| 5 mins | 2025-10-21 06:13:16.205Z | 269.262° W | 2025-10-21 06:15:16.205Z | 317.963° NNW | 31.232° | 2025-10-21 06:18:16.205Z | 31.839° NE |
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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