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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
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 (7 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-004
1 61049U 24163E   25094.47915322  .00009229  00000-0  43781-3 0  9997
2 61049  52.9773 166.0666 0009682 243.9113 116.0885 15.19941014 31013
Epoch: 2025-04-04T11:29Z
Definitive object data (Epoch: 2025-04-04T11:29:58.838Z)
Latitude
Longitude
160.5344°
Altitude
509.831 km
Speed
7.609 km/s
True Right ascension
11h 04m 15s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
5.18789°
Longitude
-26.2343°
Altitude
504.314 km
Speed
7.615 km/s
Apparent Right ascension
21h 41m 08s
Apparent Declination
-17° 02' 47"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
08:21:56
Azimuth
317.411° NNW
Elevation
-61.406°
Doppler factor
1
Orbital elements
Apogee altitude
512.969 km
Perigee altitude
499.638 km
Semi-major axis
6,884.44 km
Eccentricity
0.0009682
Inclination
52.9773°
RAAN
166.0666°
Arg. of periapsis
243.9113°
True anomaly
116.18809°
Mean anomaly
116.0885°
Eccentric anomaly
116.1383°
Mean motion
3.79962 °/min
BSTAR
0.00043781
Orbital period
94.75 mins
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SPACEMOBILE-004 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.
5 mins2025-04-05 06:35:48.331Z185.598° SSW2025-04-05 06:38:48.331Z118.294° SE25.759°2025-04-05 06:40:48.331Z78.804° E
5 mins2025-04-05 08:14:48.331Z271.72° WNW2025-04-05 08:16:48.331Z324.397° NNW31.585°2025-04-05 08:19:48.331Z32.873° NE
5 mins2025-04-05 13:13:48.331Z337.483° NNW2025-04-05 13:15:48.331Z25.626° NE28.616°2025-04-05 13:18:48.331Z91.044° ESE
5 mins2025-04-05 14:52:48.331Z276.119° WNW2025-04-05 14:54:48.331Z217.667° SW29.889°2025-04-05 14:57:48.331Z162.236° S
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