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 26283.31814077 .00003697 00000-0 18210-3 0 9998
2 61049 52.9684 139.6384 0008954 125.9064 234.2762 15.20404692115289Epoch: 2026-10-10T07:38Z
TLE epoch observation values (Epoch: 2026-10-10T07:38:07.362Z)
Latitude
-0.00004°
Longitude
6.1807°
Altitude
509.096 km
Speed
7.609 km/s
True Right ascension
09h 18m 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
18:04:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.068 km
Perigee altitude
498.742 km
Semi-major axis
6,883.042 km
Eccentricity
0.0009
Inclination
52.9684°
RAAN
139.6384°
Arg. of periapsis
125.9064°
True anomaly
234.19296°
Mean anomaly
234.2762°
Eccentric anomaly
234.23457°
Mean motion
3.80078 °/min
Orbital period
94.72 mins
BSTAR
0.0001821
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-12 01:13:28.275Z | 265.646° W | 2026-10-12 01:15:28.275Z | 233.312° WSW | 14.37° | 2026-10-12 01:17:28.275Z | 201.088° SSW |
| 5 mins | 2026-10-12 16:37:28.275Z | 222.707° SW | 2026-10-12 16:39:28.275Z | 157.814° S | 79.311° | 2026-10-12 16:42:28.275Z | 53.116° ENE |
| 4 mins | 2026-10-12 18:17:28.275Z | 314.443° NW | 2026-10-12 18:18:28.275Z | 336.311° NNW | 21.026° | 2026-10-12 18:21:28.275Z | 27.651° NE |
| 4 mins | 2026-10-12 21:36:28.275Z | 348.792° N | 2026-10-12 21:38:28.275Z | 26.514° NE | 17.531° | 2026-10-12 21:40:28.275Z | 59.828° ENE |
| 6 mins | 2026-10-12 23:14:28.275Z | 315.272° NNW | 2026-10-12 23:17:28.275Z | 69.836° E | 69.56° | 2026-10-12 23:20:28.275Z | 122.583° 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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