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: 10 hours ago
TLE from 10 hours ago
0 SPACEMOBILE-004
1 61049U 24163E 26128.01377253 .00017125 00000-0 77613-3 0 9996
2 61049 52.9662 133.6807 0009444 29.8539 330.2992 15.20931431 91655Epoch: 2026-05-08T00:19Z
TLE epoch observation values (Epoch: 2026-05-08T00:19:49.946Z)
Latitude
-0.00004°
Longitude
-97.12909°
Altitude
498.262 km
Speed
7.62 km/s
True Right ascension
08h 54m 43s
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
18:40:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.815 km
Perigee altitude
496.818 km
Semi-major axis
6,881.453 km
Eccentricity
0.00094
Inclination
52.9662°
RAAN
133.6807°
Arg. of periapsis
29.8539°
True anomaly
330.24552°
Mean anomaly
330.2992°
Eccentric anomaly
330.27237°
Mean motion
3.80209 °/min
Orbital period
94.68 mins
BSTAR
0.00077613
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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 | 2026-05-09 01:43:19.156Z | 158.902° S | 2026-05-09 01:45:19.156Z | 122.572° SE | 15.898° | 2026-05-09 01:47:19.156Z | 89.464° E |
| 5 mins | 2026-05-09 03:21:19.156Z | 251.369° W | 2026-05-09 03:23:19.156Z | 329.923° NNW | 40.865° | 2026-05-09 03:26:19.156Z | 42.159° NE |
| 4 mins | 2026-05-09 08:20:19.156Z | 349.371° N | 2026-05-09 08:22:19.156Z | 34.638° NE | 21.265° | 2026-05-09 08:24:19.156Z | 71.892° E |
| 6 mins | 2026-05-09 09:58:19.156Z | 299.869° NW | 2026-05-09 10:00:19.156Z | 260.944° W | 40.372° | 2026-05-09 10:04:19.156Z | 142.034° 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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