IRIDE FM7, 66701
Orbit data source: Space-Track
IRIDE FM7, 66701 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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66701 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
EAGLET, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.368 m²
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IRIDE FM7
1 66701U 25276AM 26147.18445059 .00007636 00000-0 35804-3 0 9993
2 66701 97.4224 221.1514 0005936 80.9109 279.2798 15.19939106 27238Epoch: 2026-05-27T04:25Z
TLE epoch observation values (Epoch: 2026-05-27T04:25:36.530Z)
Latitude
-0°
Longitude
-89.99799°
Altitude
508.458 km
Speed
7.61 km/s
True Right ascension
14h 44m 36s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:57:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.076 km
Perigee altitude
498.906 km
Semi-major axis
6,881.128 km
Eccentricity
0.00059
Inclination
97.4224°
RAAN
221.1514°
Arg. of periapsis
80.9109°
True anomaly
279.21266°
Mean anomaly
279.2798°
Eccentric anomaly
279.24623°
Mean motion
3.80236 °/min
Orbital period
94.68 mins
BSTAR
0.00035804
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Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDE FM7 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-28 04:16:11.535Z | 122.268° SE | 2026-05-28 04:19:11.535Z | 59.388° ENE | 22.361° | 2026-05-28 04:21:11.535Z | 21.092° NNE |
| 4 mins | 2026-05-28 05:51:11.535Z | 236.314° WSW | 2026-05-28 05:52:11.535Z | 256.196° W | 17.669° | 2026-05-28 05:55:11.535Z | 311.417° NW |
| 5 mins | 2026-05-28 17:21:11.535Z | 45.498° ENE | 2026-05-28 17:23:11.535Z | 106.421° ESE | 30.602° | 2026-05-28 17:26:11.535Z | 165.357° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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