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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61049 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AST & Science
Mission
Operational Commercial Communications
Bus & Motor
BW3, Unknown motor
Mass
1,500 kg wet, 1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Plate, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26185.38384721 .00016997 00000-0 77373-3 0 9996
2 61049 52.9655 229.8431 0007698 188.3855 171.7012 15.20796566100389Epoch: 2026-07-04T09:12Z
TLE epoch observation values (Epoch: 2026-07-04T09:12:44.398Z)
Latitude
-0.00002°
Longitude
169.25978°
Altitude
509.554 km
Speed
7.607 km/s
True Right ascension
15h 19m 22s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:04:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.021 km
Perigee altitude
498.426 km
Semi-major axis
6,881.86 km
Eccentricity
0.00077
Inclination
52.9655°
RAAN
229.8431°
Arg. of periapsis
188.3855°
True anomaly
171.71392°
Mean anomaly
171.7012°
Eccentric anomaly
171.70756°
Mean motion
3.80176 °/min
Orbital period
94.69 mins
BSTAR
0.00077373
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SPACEMOBILE-004 Visibility forecast
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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 mins | 2026-07-05 07:34:03.826Z | 298.67° NW | 2026-07-05 07:36:03.826Z | 331.387° NNW | 16.918° | 2026-07-05 07:39:03.826Z | 23.497° NE |
| 5 mins | 2026-07-05 12:33:03.826Z | 304.823° NW | 2026-07-05 12:35:03.826Z | 204.965° SW | 44.485° | 2026-07-05 12:38:03.826Z | 135.575° SSE |
| 5 mins | 2026-07-06 05:35:03.826Z | 242.967° WSW | 2026-07-06 05:37:03.826Z | 341.399° N | 43.338° | 2026-07-06 05:40:03.826Z | 45.527° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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