Showing default

SPACEMOBILE-005, 61046

Orbit data source: Space-Track

SPACEMOBILE-005, 61046 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
61046, 2024-163B
Orbit
LEO
Last TLE update
14 hours ago
Origin
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 (7 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Plate, 9 m
Radar Cross Section
1.500 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 14 hours ago
0 SPACEMOBILE-005
1 61046U 24163B   25094.51198563  .00005322  00000-0  25916-3 0  9999
2 61046  52.9731 166.2899 0010371 229.3475 130.6618 15.19905867 31012
Epoch: 2025-04-04T12:17Z
Definitive object data (Epoch: 2025-04-04T12:17:15.558Z)
Latitude
-0.00001°
Longitude
148.90566°
Altitude
511.657 km
Speed
7.607 km/s
True Right ascension
11h 05m 09s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
-51.4217°
Longitude
36.39464°
Altitude
517.515 km
Speed
7.608 km/s
Apparent Right ascension
23h 23m 01s
Apparent Declination
-62° 06' 11"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
07:56:35
Azimuth
216.732° SW
Elevation
-52.183°
Doppler factor
1
Orbital elements
Apogee altitude
513.55 km
Perigee altitude
499.27 km
Semi-major axis
6,884.547 km
Eccentricity
0.0010371
Inclination
52.9731°
RAAN
166.2899°
Arg. of periapsis
229.3475°
True anomaly
130.75187°
Mean anomaly
130.6618°
Eccentric anomaly
130.70684°
Mean motion
3.79953 °/min
BSTAR
0.00025916
Orbital period
94.75 mins
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

SPACEMOBILE-005 Visibility forecast

Observer location: undefined°, undefined°

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.
7 mins2025-04-05 07:23:31.986Z226.509° WSW2025-04-05 07:27:31.986Z98.472° ESE44.66°2025-04-05 07:30:31.986Z52.102° ENE
4 mins2025-04-05 09:04:31.986Z300.182° NW2025-04-05 09:06:31.986Z339.647° N19.611°2025-04-05 09:08:31.986Z17.457° NNE
4 mins2025-04-05 12:24:31.986Z349.387° N2025-04-05 12:26:31.986Z27.971° NE17.42°2025-04-05 12:28:31.986Z61.442° ENE
6 mins2025-04-05 14:02:31.986Z313.689° NW2025-04-05 14:05:31.986Z82.401° E43.702°2025-04-05 14:08:31.986Z124.912° SE
|