IRIDE FM6, 66700
Orbit data source: Space-Track
IRIDE FM6, 66700 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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66700 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: 13 hours ago
TLE from 13 hours ago
0 IRIDE FM6
1 66700U 25276AL 26141.15722234 .00004621 00000-0 21234-3 0 9999
2 66700 97.4218 215.4581 0002766 79.9155 280.2392 15.20863851 26334Epoch: 2026-05-21T03:46Z
TLE epoch observation values (Epoch: 2026-05-21T03:46:24.010Z)
Latitude
-0.00005°
Longitude
-79.94839°
Altitude
505.987 km
Speed
7.611 km/s
True Right ascension
14h 21m 49s
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
02:09:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.102 km
Perigee altitude
498.296 km
Semi-major axis
6,878.336 km
Eccentricity
0.00028
Inclination
97.4218°
RAAN
215.4581°
Arg. of periapsis
79.9155°
True anomaly
280.20801°
Mean anomaly
280.2392°
Eccentric anomaly
280.2236°
Mean motion
3.80468 °/min
Orbital period
94.62 mins
BSTAR
0.00021234
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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 FM6 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 | 2026-05-21 18:33:05.580Z | 334.733° NNW | 2026-05-21 18:35:05.580Z | 292.511° NW | 22.324° | 2026-05-21 18:38:05.580Z | 235.375° WSW |
| 5 mins | 2026-05-22 05:11:05.580Z | 186.39° SSW | 2026-05-22 05:13:05.580Z | 291.555° WNW | 40.889° | 2026-05-22 05:16:05.580Z | 340.911° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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