IRIDE-MS2-HEO-2, 64569
Orbit data source: Space-Track
IRIDE-MS2-HEO-2, 64569 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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64569 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: 7 hours ago
TLE from 7 hours ago
0 IRIDE-MS2-HEO-2
1 64569U 25135AT 26072.92135189 .00003313 00000-0 32219-3 0 9991
2 64569 97.7621 188.3319 0000874 10.1308 349.9929 14.93246219 39669Epoch: 2026-03-13T22:06Z
TLE epoch observation values (Epoch: 2026-03-13T22:06:44.803Z)
Latitude
-0.00002°
Longitude
45.09527°
Altitude
590.266 km
Speed
7.565 km/s
True Right ascension
12h 33m 19s
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
09:44:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.447 km
Perigee altitude
584.23 km
Semi-major axis
6,962.976 km
Eccentricity
0.00009
Inclination
97.7621°
RAAN
188.3319°
Arg. of periapsis
10.1308°
True anomaly
349.99116°
Mean anomaly
349.9929°
Eccentric anomaly
349.99203°
Mean motion
3.73552 °/min
Orbital period
96.37 mins
BSTAR
0.00032219
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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-2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-14 07:53:45.515Z | 185.007° SSW | 2026-03-14 07:56:45.515Z | 288.855° WNW | 39.571° | 2026-03-14 07:59:45.515Z | 337.786° N |
| 4 mins | 2026-03-14 19:37:45.515Z | 70.311° E | 2026-03-14 19:38:45.515Z | 89.67° E | 19.265° | 2026-03-14 19:41:45.515Z | 140.093° SSE |
| 5 mins | 2026-03-14 21:12:45.515Z | 329.904° NNW | 2026-03-14 21:14:45.515Z | 281.278° WNW | 26.209° | 2026-03-14 21:17:45.515Z | 230.96° WSW |
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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