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: 18 hours ago
TLE from 18 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26037.66666544 .00017630 00000-0 79294-3 0 9998
2 61049 52.9676 189.3153 0011335 123.5928 236.6150 15.21155742 77909Epoch: 2026-02-06T15:59Z
TLE epoch observation values (Epoch: 2026-02-06T15:59:59.894Z)
Latitude
0.00002°
Longitude
172.51449°
Altitude
507.526 km
Speed
7.609 km/s
True Right ascension
12h 37m 15s
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
12:23:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.439 km
Perigee altitude
494.84 km
Semi-major axis
6,880.777 km
Eccentricity
0.00113
Inclination
52.9676°
RAAN
189.3153°
Arg. of periapsis
123.5928°
True anomaly
236.50663°
Mean anomaly
236.615°
Eccentric anomaly
236.56081°
Mean motion
3.80266 °/min
Orbital period
94.67 mins
BSTAR
0.00079294
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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 | 2026-02-07 12:40:27.081Z | 226.775° WSW | 2026-02-07 12:43:27.081Z | 211.786° SW | 43.445° | 2026-02-07 12:47:27.081Z | 51.608° ENE |
| 4 mins | 2026-02-07 14:21:27.081Z | 310.351° NW | 2026-02-07 14:22:27.081Z | 330.945° NNW | 18.875° | 2026-02-07 14:25:27.081Z | 25.098° NE |
| 5 mins | 2026-02-07 19:19:27.081Z | 316.226° NNW | 2026-02-07 19:21:27.081Z | 73.731° E | 44.013° | 2026-02-07 19:24:27.081Z | 125.045° SE |
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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