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: 12 hours ago
TLE from 12 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26035.69559619 .00007767 00000-0 35797-3 0 9993
2 61049 52.9676 198.3844 0011703 119.2825 240.9340 15.21156126 77606Epoch: 2026-02-04T16:41Z
TLE epoch observation values (Epoch: 2026-02-04T16:41:39.510Z)
Latitude
-0.00008°
Longitude
173.11124°
Altitude
507.147 km
Speed
7.61 km/s
True Right ascension
13h 13m 32s
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
06:45:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.691 km
Perigee altitude
494.586 km
Semi-major axis
6,880.776 km
Eccentricity
0.00117
Inclination
52.9676°
RAAN
198.3844°
Arg. of periapsis
119.2825°
True anomaly
240.81687°
Mean anomaly
240.934°
Eccentric anomaly
240.87542°
Mean motion
3.80266 °/min
Orbital period
94.67 mins
BSTAR
0.00035797
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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 | 2026-02-05 13:21:46.124Z | 225.201° WSW | 2026-02-05 13:25:46.124Z | 76.127° E | 43.073° | 2026-02-05 13:28:46.124Z | 52.65° ENE |
| 4 mins | 2026-02-05 15:02:46.124Z | 305.345° NW | 2026-02-05 15:04:46.124Z | 347.987° N | 19.02° | 2026-02-05 15:06:46.124Z | 22.533° NE |
| 5 mins | 2026-02-05 20:00:46.124Z | 316.932° NNW | 2026-02-05 20:02:46.124Z | 24.362° NE | 43.78° | 2026-02-05 20:05:46.124Z | 122.703° 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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