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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
15 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 (8 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, 9 m
Radar Cross Section
1.500 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 15 hours ago
0 SPACEMOBILE-005
1 61046U 24163B   25133.83236286  .00000073  00000-0  18288-4 0  9996
2 61046  52.9762 345.7124 0010208   1.9999 358.1034 15.20154131 36998
Epoch: 2025-05-13T19:58Z
Definitive object data (Epoch: 2025-05-13T19:58:36.151Z)
Latitude
-0.00001°
Longitude
174.23633°
Altitude
499.229 km
Speed
7.62 km/s
True Right ascension
23h 02m 50s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
53.113°
Longitude
-100.4586°
Altitude
511.266 km
Speed
7.615 km/s
Apparent Right ascension
05h 59m 37s
Apparent Declination
9° 19' 02"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:03:12
Azimuth
20.233° NNE
Elevation
-38.612°
Doppler factor
1
Orbital elements
Apogee altitude
512.687 km
Perigee altitude
498.633 km
Semi-major axis
6,883.797 km
Eccentricity
0.0010208
Inclination
52.9762°
RAAN
345.7124°
Arg. of periapsis
1.9999°
True anomaly
358.09952°
Mean anomaly
358.1034°
Eccentric anomaly
358.10146°
Mean motion
3.80015 °/min
BSTAR
0.000018288
Orbital period
94.73 mins
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SPACEMOBILE-005 Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
6 mins2025-05-14 16:39:58.533Z221.65° SW2025-05-14 16:42:58.533Z140.135° SSE43.878°2025-05-14 16:45:58.533Z54.767° ENE
4 mins2025-05-14 18:19:58.533Z297.086° NW2025-05-14 18:21:58.533Z337.625° N20.252°2025-05-14 18:23:58.533Z17.098° NNE
4 mins2025-05-14 21:39:58.533Z349.35° N2025-05-14 21:41:58.533Z26.931° NE16.534°2025-05-14 21:43:58.533Z59.547° ENE
6 mins2025-05-14 23:17:58.533Z316.306° NNW2025-05-14 23:20:58.533Z65.166° ENE42.591°2025-05-14 23:23:58.533Z120.781° SE
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