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SPACEMOBILE-005, 61046

Orbit data source: Space-Track

SPACEMOBILE-005, 61046 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
61046, 2024-163B
Orbit
LEO
Last TLE update
10 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 10 hours ago
0 SPACEMOBILE-005
1 61046U 24163B   25199.57132896  .00003403  00000-0  16872-3 0  9997
2 61046  52.9749  43.6473 0010122 187.6322 172.4519 15.20418302 46990
Epoch: 2025-07-18T13:42Z
TLE epoch observation values (Epoch: 2025-07-18T13:42:42.822Z)
Latitude
-0.00005°
Longitude
-98.65204°
Altitude
512.36 km
Speed
7.605 km/s
True Right ascension
02h 54m 35s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
50.76581°
Longitude
12.72794°
Altitude
509.863 km
Speed
7.616 km/s
Apparent Right ascension
04h 36m 37s
Apparent Declination
25° 51' 48"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:25:47
Azimuth
306.85° NW
Elevation
-2.094°
Doppler factor
1
Orbital elements
Apogee altitude
511.83 km
Perigee altitude
497.896 km
Semi-major axis
6,883 km
Eccentricity
0.00101
Inclination
52.9749°
RAAN
43.6473°
Arg. of periapsis
187.6322°
True anomaly
172.46712°
Mean anomaly
172.4519°
Eccentric anomaly
172.45951°
Mean motion
3.80081 °/min
Orbital period
94.72 mins
BSTAR
0.00016872
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