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: 22 hours ago
TLE from 22 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 25312.51760311 .00006009 00000-0 28192-3 0 9993
2 61049 52.9771 244.0260 0010007 188.0090 172.0746 15.20974438 64184Epoch: 2025-11-08T12:25Z
TLE epoch observation values (Epoch: 2025-11-08T12:25:20.908Z)
Latitude
-0.00004°
Longitude
9.74278°
Altitude
510.597 km
Speed
7.606 km/s
True Right ascension
16h 16m 06s
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
06:33:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.071 km
Perigee altitude
496.299 km
Semi-major axis
6,881.322 km
Eccentricity
0.001
Inclination
52.9771°
RAAN
244.026°
Arg. of periapsis
188.009°
True anomaly
172.09039°
Mean anomaly
172.0746°
Eccentric anomaly
172.0825°
Mean motion
3.8022 °/min
Orbital period
94.68 mins
BSTAR
0.00028192
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-09 21:41:47.456Z | 213.164° SW | 2025-11-09 21:45:47.456Z | 119.133° SE | 38.544° | 2025-11-09 21:48:47.456Z | 60.359° ENE |
| 4 mins | 2025-11-09 23:22:47.456Z | 297.88° NW | 2025-11-09 23:23:47.456Z | 320.215° NNW | 22.888° | 2025-11-09 23:26:47.456Z | 23.943° NE |
| 5 mins | 2025-11-10 04:20:47.456Z | 326.228° NNW | 2025-11-10 04:22:47.456Z | 19.685° NNE | 37.705° | 2025-11-10 04:25:47.456Z | 108.227° ESE |
| 4 mins | 2025-11-10 05:59:47.456Z | 261.621° W | 2025-11-10 06:00:47.456Z | 242.356° WSW | 18.231° | 2025-11-10 06:03:47.456Z | 187.036° SSW |
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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