Showing default

IRIDE-MS2-HEO-5, 64571

Orbit data source: Space-Track

IRIDE-MS2-HEO-5, 64571 is an Italian payload satellite in SSO that was launched on Mon, 23 Jun 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
64571, 2025-135AV
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
ArgoTec
Mission
Operational Civil Imaging
Bus & Motor
HAWK, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
2025-06-23 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
0.683 m², Medium (>0.1 m² and < 1m²)

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

TLE from 6 hours ago
0 IRIDE-MS2-HEO-5
1 64571U 25135AV  26062.57232597  .00003286  00000-0  31799-3 0  9996
2 64571  97.7593 178.1049 0001762 324.2097  35.9004 14.93447582 38120
Epoch: 2026-03-03T13:44Z
TLE epoch observation values (Epoch: 2026-03-03T13:44:08.963Z)
Latitude
-0.00008°
Longitude
170.71811°
Altitude
589.245 km
Speed
7.566 km/s
True Right ascension
11h 52m 25s
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
23:37:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.439 km
Perigee altitude
582.985 km
Semi-major axis
6,962.349 km
Eccentricity
0.00018
Inclination
97.7593°
RAAN
178.1049°
Arg. of periapsis
324.2097°
True anomaly
35.91224°
Mean anomaly
35.9004°
Eccentric anomaly
35.90632°
Mean motion
3.73602 °/min
Orbital period
96.36 mins
BSTAR
0.00031799
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
|