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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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Identifier
61049, 2024-163E
Orbit
LEO
Country
Flag of USUS
Related 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)
2024-09-12 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Plate, 4.5 m
Radar Cross Section
1.500 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 SPACEMOBILE-004
1 61049U 24163E   25241.21004482  .00005826  00000-0  27679-3 0  9996
2 61049  52.9785 211.8756 0010478 352.0376   8.0451 15.20589656 53333
Epoch: 2025-08-29T05:02Z
TLE epoch observation values (Epoch: 2025-08-29T05:02:27.872Z)
Latitude
0.00004°
Longitude
158.59753°
Altitude
497.797 km
Speed
7.621 km/s
True Right ascension
14h 07m 30s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:27:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.557 km
Perigee altitude
497.134 km
Semi-major axis
6,882.482 km
Eccentricity
0.00105
Inclination
52.9785°
RAAN
211.8756°
Arg. of periapsis
352.0376°
True anomaly
8.06193°
Mean anomaly
8.0451°
Eccentric anomaly
8.05351°
Mean motion
3.80124 °/min
Orbital period
94.71 mins
BSTAR
0.00027679
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