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.
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64576 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
ArgoTec
Mission
Operational Civil Imaging
Bus & Motor
HAWK, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 IRIDE-MS2-HEO-6
1 64576U 25135BA 26235.90945986 .00001301 00000-0 13407-3 0 9995
2 64576 97.7777 349.2010 0002625 107.7315 252.4190 14.91945677 63984Epoch: 2026-08-23T21:49Z
TLE epoch observation values (Epoch: 2026-08-23T21:49:37.331Z)
Latitude
-0.0001°
Longitude
49.59672°
Altitude
595.464 km
Speed
7.562 km/s
True Right ascension
23h 16m 48s
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
21:42:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.718 km
Perigee altitude
587.06 km
Semi-major axis
6,967.026 km
Eccentricity
0.00026
Inclination
97.7777°
RAAN
349.201°
Arg. of periapsis
107.7315°
True anomaly
252.39033°
Mean anomaly
252.419°
Eccentric anomaly
252.40466°
Mean motion
3.73226 °/min
Orbital period
96.46 mins
BSTAR
0.00013407
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-MS2-HEO-6 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-24 07:36:24.009Z | 164.164° S | 2026-08-24 07:40:24.009Z | 0.454° NNE | 42.961° | 2026-08-24 07:43:24.009Z | 349.133° N |
| 6 mins | 2026-08-24 20:56:24.009Z | 350.234° N | 2026-08-24 20:58:24.009Z | 305.614° NW | 34.928° | 2026-08-24 21:02:24.009Z | 215.536° SW |
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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