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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
Last TLE update
1 day 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 1 day ago
0 SPACEMOBILE-004
1 61049U 24163E   25198.02584553  .00001357  00000-0  76185-4 0  9990
2 61049  52.9783  50.3726 0010003 196.9323 163.1339 15.20445596 46766
Epoch: 2025-07-17T00:37Z
TLE epoch observation values (Epoch: 2025-07-17T00:37:13.053Z)
Latitude
-0.00001°
Longitude
105.97063°
Altitude
511.961 km
Speed
7.605 km/s
True Right ascension
03h 21m 29s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-21.58523°
Longitude
82.08506°
Altitude
515.091 km
Speed
7.604 km/s
Apparent Right ascension
04h 55m 21s
Apparent Declination
-65° 22' 43"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
23:58:02
Azimuth
152.467° SSE
Elevation
-29.802°
Doppler factor
1
Orbital elements
Apogee altitude
511.665 km
Perigee altitude
497.895 km
Semi-major axis
6,882.917 km
Eccentricity
0.001
Inclination
52.9783°
RAAN
50.3726°
Arg. of periapsis
196.9323°
True anomaly
163.16712°
Mean anomaly
163.1339°
Eccentric anomaly
163.15051°
Mean motion
3.80088 °/min
Orbital period
94.71 mins
BSTAR
0.000076185
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