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IRIDE FM2, 66696

Orbit data source: Space-Track

IRIDE FM2, 66696 is an Italian payload satellite in SSO that was launched on Fri, 28 Nov 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.

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Identifier
66696, 2025-276AG
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
2025-11-28 (4 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, 1.0 m
Radar Cross Section
0.368 m²

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 IRIDE FM2
1 66696U 25276AG  26092.19725721  .00011978  00000-0  56820-3 0  9998
2 66696  97.4226 167.0258 0002132 274.1150  85.9841 15.19421492 18880
Epoch: 2026-04-02T04:44Z
TLE epoch observation values (Epoch: 2026-04-02T04:44:03.022Z)
Latitude
-0.00006°
Longitude
-94.53598°
Altitude
510.574 km
Speed
7.609 km/s
True Right ascension
11h 08m 06s
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
03:04:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.023 km
Perigee altitude
503.088 km
Semi-major axis
6,882.692 km
Eccentricity
0.00021
Inclination
97.4226°
RAAN
167.0258°
Arg. of periapsis
274.115°
True anomaly
86.00847°
Mean anomaly
85.9841°
Eccentric anomaly
85.99629°
Mean motion
3.80107 °/min
Orbital period
94.71 mins
BSTAR
0.0005682
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