Showing default

AE1D, 62618

Orbit data source: Space-Track

AE1D, 62618 is a payload satellite owned by ArkEdge (JP) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
62618, 2025-009K
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
ArkEdge
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2025-01-14 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 AE1D
1 62618U 25009K   26104.17598394  .00039458  00000-0  66889-3 0  9997
2 62618  97.3970 191.7675 0004486 180.4213 179.7036 15.51410373 69498
Epoch: 2026-04-14T04:13Z
TLE epoch observation values (Epoch: 2026-04-14T04:13:25.012Z)
Latitude
-0.00003°
Longitude
-73.94271°
Altitude
418.787 km
Speed
7.658 km/s
True Right ascension
12h 47m 04s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
19:14:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
412.576 km
Perigee altitude
406.486 km
Semi-major axis
6,787.668 km
Eccentricity
0.00045
Inclination
97.397°
RAAN
191.7675°
Arg. of periapsis
180.4213°
True anomaly
179.70387°
Mean anomaly
179.7036°
Eccentric anomaly
179.70373°
Mean motion
3.88117 °/min
Orbital period
92.76 mins
BSTAR
0.00066889
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
|