DECAYED
Showing default

ICEYE-X15, 48917 (Decayed)

Orbit data source: Space-Track

ICEYE-X15, 48917 was a payload satellite owned by ICEYE (FI) in LEO that was launched on Wed, 30 Jun 2021 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.

Not visible in the next 10 days
Identifier
48917, 2021-059AQ
Orbit
Decayed
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Decayed Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2021-06-30 (5 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 months ago

TLE from 6 months ago
0 ICEYE-X15
1 48917U 21059AQ  25224.50156410  .05947204  26974-5  40307-3 0  9994
2 48917  97.6213  55.6369 0009994 259.0179 100.9996 16.40666032231191
Epoch: 2025-08-12T12:02Z
TLE epoch observation values (Epoch: 2025-08-12T12:02:15.138Z)
Latitude
-0.00001°
Longitude
-86.11947°
Altitude
168.531 km
Speed
7.804 km/s
True Right ascension
03h 42m 32s
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
19:00:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.383 km
Perigee altitude
154.313 km
Semi-major axis
6,538.985 km
Eccentricity
0.001
Inclination
97.6213°
RAAN
55.6369°
Arg. of periapsis
259.0179°
True anomaly
101.11199°
Mean anomaly
100.9996°
Eccentric anomaly
101.0558°
Mean motion
4.10466 °/min
Orbital period
87.71 mins
BSTAR
0.00040307
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
|