Showing default

IRIDE-MS2-HEO-6, 64576

Orbit data source: Space-Track

IRIDE-MS2-HEO-6, 64576 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
64576, 2025-135BA
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 (5 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: 5 hours ago

TLE from 5 hours ago
0 IRIDE-MS2-HEO-6
1 64576U 25135BA  25328.57522858  .00002806  00000-0  27605-3 0  9995
2 64576  97.7578  80.4722 0002326 287.6906  72.4059 14.92900595 23351
Epoch: 2025-11-24T13:48Z
TLE epoch observation values (Epoch: 2025-11-24T13:48:19.749Z)
Latitude
-0.00004°
Longitude
169.61669°
Altitude
591.45 km
Speed
7.565 km/s
True Right ascension
05h 21m 53s
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
15:50:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.534 km
Perigee altitude
584.294 km
Semi-major axis
6,964.051 km
Eccentricity
0.00023
Inclination
97.7578°
RAAN
80.4722°
Arg. of periapsis
287.6906°
True anomaly
72.43131°
Mean anomaly
72.4059°
Eccentric anomaly
72.4186°
Mean motion
3.73465 °/min
Orbital period
96.39 mins
BSTAR
0.00027605
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
|