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SPACEMOBILE-001, 61047

Orbit data source: Space-Track

SPACEMOBILE-001, 61047 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
61047, 2024-163C
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, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 SPACEMOBILE-001
1 61047U 24163C   26034.87394516  .00001437  00000-0  78416-4 0  9997
2 61047  52.9736 202.3285 0010939  89.5945 270.6303 15.21100120 77475
Epoch: 2026-02-03T20:58Z
TLE epoch observation values (Epoch: 2026-02-03T20:58:28.861Z)
Latitude
-0.00002°
Longitude
113.65961°
Altitude
503.323 km
Speed
7.614 km/s
True Right ascension
13h 29m 18s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
06:44:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.334 km
Perigee altitude
495.279 km
Semi-major axis
6,880.943 km
Eccentricity
0.00109
Inclination
52.9736°
RAAN
202.3285°
Arg. of periapsis
89.5945°
True anomaly
270.50495°
Mean anomaly
270.6303°
Eccentric anomaly
270.56763°
Mean motion
3.80252 °/min
Orbital period
94.67 mins
BSTAR
0.000078416
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Documentation

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