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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
Last TLE update
16 hours ago
Origin
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 (10 months 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

TLE from 16 hours ago
0 SPACEMOBILE-001
1 61047U 24163C   25199.30835075  .00003485  00000-0  17246-3 0  9994
2 61047  52.9713  44.7264 0010142 186.8291 173.2566 15.20415579 46950
Epoch: 2025-07-18T07:24Z
TLE epoch observation values (Epoch: 2025-07-18T07:24:01.504Z)
Latitude
-0.00007°
Longitude
-2.64159°
Altitude
512.394 km
Speed
7.605 km/s
True Right ascension
02h 58m 54s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
49.85692°
Longitude
111.43396°
Altitude
509.335 km
Speed
7.616 km/s
Apparent Right ascension
04h 46m 45s
Apparent Declination
27° 06' 18"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:26:25
Azimuth
306.164° NW
Elevation
0.271°
Doppler factor
1
Orbital elements
Apogee altitude
511.853 km
Perigee altitude
497.891 km
Semi-major axis
6,883.009 km
Eccentricity
0.00101
Inclination
52.9713°
RAAN
44.7264°
Arg. of periapsis
186.8291°
True anomaly
173.27023°
Mean anomaly
173.2566°
Eccentric anomaly
173.26342°
Mean motion
3.80081 °/min
Orbital period
94.72 mins
BSTAR
0.00017246
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