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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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: 8 hours ago
TLE from 8 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26095.22379648 .00018900 00000-0 85245-3 0 9994
2 61049 52.9773 284.5077 0006730 293.9093 66.1196 15.21045152 86660Epoch: 2026-04-05T05:22Z
TLE epoch observation values (Epoch: 2026-04-05T05:22:16.015Z)
Latitude
-0.00004°
Longitude
10.40864°
Altitude
501.691 km
Speed
7.616 km/s
True Right ascension
18h 58m 01s
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
19:30:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.603 km
Perigee altitude
498.341 km
Semi-major axis
6,881.109 km
Eccentricity
0.00067
Inclination
52.9773°
RAAN
284.5077°
Arg. of periapsis
293.9093°
True anomaly
66.19014°
Mean anomaly
66.1196°
Eccentric anomaly
66.15487°
Mean motion
3.80238 °/min
Orbital period
94.68 mins
BSTAR
0.00085245
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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 | 2026-04-05 14:59:18.441Z | 209.921° SW | 2026-04-05 15:03:18.441Z | 113.967° SE | 36.126° | 2026-04-05 15:06:18.441Z | 61.491° ENE |
| 4 mins | 2026-04-05 16:40:18.441Z | 299.27° NW | 2026-04-05 16:41:18.441Z | 323.737° NNW | 24.158° | 2026-04-05 16:44:18.441Z | 26.449° NE |
| 5 mins | 2026-04-05 21:38:18.441Z | 329.869° NNW | 2026-04-05 21:40:18.441Z | 29.859° NE | 36.664° | 2026-04-05 21:43:18.441Z | 106.249° ESE |
| 4 mins | 2026-04-05 23:17:18.441Z | 260.543° W | 2026-04-05 23:18:18.441Z | 239.731° WSW | 20.121° | 2026-04-05 23:21:18.441Z | 183.296° SSW |
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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