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: 6 hours ago
TLE from 6 hours ago
0 IRIDE-MS2-HEO-6
1 64576U 25135BA 26260.25482986 .00001552 00000-0 15883-3 0 9995
2 64576 97.7801 13.2294 0002134 73.9484 286.1970 14.91944970 67619Epoch: 2026-09-17T06:06Z
TLE epoch observation values (Epoch: 2026-09-17T06:06:57.299Z)
Latitude
-0.00002°
Longitude
-74.70404°
Altitude
594.498 km
Speed
7.563 km/s
True Right ascension
00h 52m 55s
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
05:12:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.378 km
Perigee altitude
587.404 km
Semi-major axis
6,967.028 km
Eccentricity
0.00021
Inclination
97.7801°
RAAN
13.2294°
Arg. of periapsis
73.9484°
True anomaly
286.17352°
Mean anomaly
286.197°
Eccentric anomaly
286.18526°
Mean motion
3.73226 °/min
Orbital period
96.46 mins
BSTAR
0.00015883
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 19:34:37.013Z | 48.942° ENE | 2026-09-17 19:37:37.013Z | 97.186° ESE | 19.495° | 2026-09-17 19:39:37.013Z | 131.123° SE |
| 6 mins | 2026-09-17 21:10:37.013Z | 341.203° N | 2026-09-17 21:12:37.013Z | 302.007° NW | 31.203° | 2026-09-17 21:16:37.013Z | 227.19° WSW |
| 6 mins | 2026-09-18 08:00:37.013Z | 195.21° SSW | 2026-09-18 08:02:37.013Z | 252.09° W | 50.806° | 2026-09-18 08:06:37.013Z | 336.261° NNW |
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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