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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SPACEMOBILE-004 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: 18 hours ago
TLE from 18 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 25258.03580478 -.00000618 00000-0 -12980-4 0 9994
2 61049 52.9755 134.5299 0011064 40.4911 319.6904 15.20528005 55896Epoch: 2025-09-15T00:51Z
TLE epoch observation values (Epoch: 2025-09-15T00:51:33.533Z)
Latitude
-0.00003°
Longitude
127.39392°
Altitude
499.32 km
Speed
7.619 km/s
True Right ascension
08h 58m 07s
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
11:39:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.147 km
Perigee altitude
496.917 km
Semi-major axis
6,882.669 km
Eccentricity
0.00111
Inclination
52.9755°
RAAN
134.5299°
Arg. of periapsis
40.4911°
True anomaly
319.60829°
Mean anomaly
319.6904°
Eccentric anomaly
319.64936°
Mean motion
3.80109 °/min
Orbital period
94.71 mins
BSTAR
-0.00001298
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 20:02:16.483Z | 284.912° WNW | 2025-09-15 20:05:16.483Z | 342.485° N | 20.962° | 2025-09-15 20:07:16.483Z | 20.615° NNE |
| 6 mins | 2025-09-16 01:01:16.483Z | 320.153° NNW | 2025-09-16 01:03:16.483Z | 358.55° N | 39.503° | 2025-09-16 01:07:16.483Z | 117.894° SE |
| 6 mins | 2025-09-16 18:03:16.483Z | 217.924° SW | 2025-09-16 18:06:16.483Z | 102.199° ESE | 41.974° | 2025-09-16 18:09:16.483Z | 55.633° ENE |
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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