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: 2 days ago
TLE from 2 days ago
0 SPACEMOBILE-004
1 61049U 24163E 26225.73786682 .00008544 00000-0 39988-3 0 9991
2 61049 52.9739 44.3062 0006086 327.2665 32.7951 15.20526923106523Epoch: 2026-08-13T17:42Z
TLE epoch observation values (Epoch: 2026-08-13T17:42:31.693Z)
Latitude
-0.00003°
Longitude
176.50098°
Altitude
501.606 km
Speed
7.617 km/s
True Right ascension
02h 57m 13s
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
13:22:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.724 km
Perigee altitude
500.347 km
Semi-major axis
6,882.672 km
Eccentricity
0.00061
Inclination
52.9739°
RAAN
44.3062°
Arg. of periapsis
327.2665°
True anomaly
32.8329°
Mean anomaly
32.7951°
Eccentric anomaly
32.814°
Mean motion
3.80108 °/min
Orbital period
94.71 mins
BSTAR
0.00039988
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-16 13:43:00.076Z | 216.286° SW | 2026-08-16 13:46:00.076Z | 120.575° SE | 41.936° | 2026-08-16 13:49:00.076Z | 57.109° ENE |
| 4 mins | 2026-08-16 15:23:00.076Z | 298.374° NW | 2026-08-16 15:25:00.076Z | 342.842° N | 21.331° | 2026-08-16 15:27:00.076Z | 20.846° NNE |
| 6 mins | 2026-08-16 20:21:00.076Z | 320.479° NNW | 2026-08-16 20:23:00.076Z | 359.19° N | 39.37° | 2026-08-16 20:27:00.076Z | 117.435° SE |
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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