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: 20 hours ago
TLE from 20 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26307.64176342 .00005119 00000-0 24776-3 0 9992
2 61049 52.9738 27.8594 0006819 189.7088 170.3775 15.20215909118987Epoch: 2026-11-03T15:24Z
TLE epoch observation values (Epoch: 2026-11-03T15:24:08.359Z)
Latitude
-0.00004°
Longitude
113.92303°
Altitude
510.692 km
Speed
7.607 km/s
True Right ascension
01h 51m 26s
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
06:59:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.168 km
Perigee altitude
500.78 km
Semi-major axis
6,883.611 km
Eccentricity
0.00068
Inclination
52.9738°
RAAN
27.8594°
Arg. of periapsis
189.7088°
True anomaly
170.39055°
Mean anomaly
170.3775°
Eccentric anomaly
170.38403°
Mean motion
3.80031 °/min
Orbital period
94.73 mins
BSTAR
0.00024776
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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 | 2026-11-04 13:58:08.286Z | 340.332° N | 2026-11-04 14:00:08.286Z | 27.564° NE | 30.031° | 2026-11-04 14:03:08.286Z | 88.066° E |
| 5 mins | 2026-11-04 15:37:08.286Z | 279.547° WNW | 2026-11-04 15:39:08.286Z | 213.128° SW | 40.163° | 2026-11-04 15:42:08.286Z | 157.33° SSE |
| 5 mins | 2026-11-05 07:01:08.286Z | 171.721° S | 2026-11-05 07:03:08.286Z | 123.031° SE | 27.234° | 2026-11-05 07:06:08.286Z | 72.209° E |
| 5 mins | 2026-11-05 08:39:08.286Z | 267.9° W | 2026-11-05 08:41:08.286Z | 318.999° NNW | 39.859° | 2026-11-05 08:44:08.286Z | 32.816° 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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