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: 8 hours ago
TLE from 8 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26093.58110324 .00032912 00000-0 14707-2 0 9998
2 61049 52.9778 292.0643 0005666 291.2627 68.7762 15.21052851 86413Epoch: 2026-04-03T13:56Z
TLE epoch observation values (Epoch: 2026-04-03T13:56:47.319Z)
Latitude
-0.00005°
Longitude
-109.04608°
Altitude
502.131 km
Speed
7.615 km/s
True Right ascension
19h 28m 15s
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
03:39:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.847 km
Perigee altitude
499.05 km
Semi-major axis
6,881.085 km
Eccentricity
0.00057
Inclination
52.9778°
RAAN
292.0643°
Arg. of periapsis
291.2627°
True anomaly
68.83674°
Mean anomaly
68.7762°
Eccentric anomaly
68.80647°
Mean motion
3.8024 °/min
Orbital period
94.68 mins
BSTAR
0.0014707
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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 | 2026-04-03 22:18:33.784Z | 322.318° NNW | 2026-04-03 22:21:33.784Z | 26.526° NE | 35.567° | 2026-04-03 22:24:33.784Z | 104.012° ESE |
| 4 mins | 2026-04-03 23:58:33.784Z | 262.818° W | 2026-04-03 23:59:33.784Z | 241.819° WSW | 20.913° | 2026-04-04 00:02:33.784Z | 182.6° SSW |
| 5 mins | 2026-04-04 15:21:33.784Z | 197.562° SSW | 2026-04-04 15:23:33.784Z | 133.907° SE | 36.376° | 2026-04-04 15:26:33.784Z | 63.864° ENE |
| 4 mins | 2026-04-04 17:00:33.784Z | 292.164° WNW | 2026-04-04 17:02:33.784Z | 342.328° N | 24.425° | 2026-04-04 17:04:33.784Z | 22.75° NE |
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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