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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Edit Public Description
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: 19 hours ago
TLE from 19 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 25342.61231089 .00025358 00000-0 11406-2 0 9999
2 61049 52.9704 105.5877 0009465 295.9264 64.0754 15.20939975 68766Epoch: 2025-12-08T14:41Z
TLE epoch observation values (Epoch: 2025-12-08T14:41:43.660Z)
Latitude
-0.00008°
Longitude
167.54688°
Altitude
501.037 km
Speed
7.617 km/s
True Right ascension
07h 02m 21s
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
07:42:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.803 km
Perigee altitude
496.777 km
Semi-major axis
6,881.427 km
Eccentricity
0.00095
Inclination
52.9704°
RAAN
105.5877°
Arg. of periapsis
295.9264°
True anomaly
64.173°
Mean anomaly
64.0754°
Eccentric anomaly
64.12419°
Mean motion
3.80212 °/min
Orbital period
94.68 mins
BSTAR
0.0011406
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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 | 2025-12-09 09:46:05.695Z | 164.401° S | 2025-12-09 09:48:05.695Z | 132.492° SE | 15.184° | 2025-12-09 09:50:05.695Z | 97.377° ESE |
| 6 mins | 2025-12-09 11:24:05.695Z | 244.937° WSW | 2025-12-09 11:26:05.695Z | 284.157° WNW | 40.394° | 2025-12-09 11:30:05.695Z | 44.746° NE |
| 4 mins | 2025-12-09 16:24:05.695Z | 358.284° N | 2025-12-09 16:25:05.695Z | 20.885° NNE | 21.15° | 2025-12-09 16:28:05.695Z | 75.694° E |
| 5 mins | 2025-12-09 18:02:05.695Z | 299.655° NW | 2025-12-09 18:04:05.695Z | 222.131° SW | 43.03° | 2025-12-09 18:07:05.695Z | 141.136° SSE |
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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