Showing default

SPACEMOBILE-002, 61048

Orbit data source: Space-Track

SPACEMOBILE-002, 61048 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.

Loading next visibility...
Identifier
61048, 2024-163D
Orbit
LEO
Country
Flag of USUS
Related 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)
2024-09-12 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Plate, 6.5 m
Radar Cross Section
32.590 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 SPACEMOBILE-002
1 61048U 24163D   26074.87059190  .00013446  00000-0  60978-3 0  9994
2 61048  52.9825  18.3120 0006331 190.5167 169.5696 15.21122471 83569
Epoch: 2026-03-15T20:53Z
TLE epoch observation values (Epoch: 2026-03-15T20:53:39.140Z)
Latitude
-0.00001°
Longitude
-108.5723°
Altitude
507.615 km
Speed
7.609 km/s
True Right ascension
01h 13m 14s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:36:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.094 km
Perigee altitude
498.381 km
Semi-major axis
6,880.875 km
Eccentricity
0.00063
Inclination
52.9825°
RAAN
18.312°
Arg. of periapsis
190.5167°
True anomaly
169.58272°
Mean anomaly
169.5696°
Eccentric anomaly
169.57616°
Mean motion
3.80257 °/min
Orbital period
94.67 mins
BSTAR
0.00060978
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|