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: 13 hours ago
TLE from 13 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26235.40019277 .00013842 00000-0 63807-3 0 9999
2 61049 52.9709 359.8916 0006462 358.0024 2.0943 15.20532597107998Epoch: 2026-08-23T09:36Z
TLE epoch observation values (Epoch: 2026-08-23T09:36:16.655Z)
Latitude
-0.00003°
Longitude
-115.87461°
Altitude
500.664 km
Speed
7.618 km/s
True Right ascension
23h 59m 33s
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
14:02:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.966 km
Perigee altitude
500.071 km
Semi-major axis
6,882.656 km
Eccentricity
0.00065
Inclination
52.9709°
RAAN
359.8916°
Arg. of periapsis
358.0024°
True anomaly
2.09701°
Mean anomaly
2.0943°
Eccentric anomaly
2.09565°
Mean motion
3.8011 °/min
Orbital period
94.71 mins
BSTAR
0.00063807
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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 | 2026-08-24 11:01:49.435Z | 228.532° WSW | 2026-08-24 11:04:49.435Z | 59.144° ENE | 44.585° | 2026-08-24 11:07:49.435Z | 50.739° ENE |
| 4 mins | 2026-08-24 12:41:49.435Z | 302.856° NW | 2026-08-24 12:43:49.435Z | 342.439° N | 18.683° | 2026-08-24 12:45:49.435Z | 18.859° NNE |
| 4 mins | 2026-08-24 16:01:49.435Z | 352.832° N | 2026-08-24 16:02:49.435Z | 11.927° NNE | 17.655° | 2026-08-24 16:05:49.435Z | 65.09° ENE |
| 6 mins | 2026-08-24 17:39:49.435Z | 312.661° NW | 2026-08-24 17:41:49.435Z | 328.085° NNW | 42.486° | 2026-08-24 17:45:49.435Z | 127.349° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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