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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS2-HEO-2
1 64569U 25135AT 25328.19944466 .00003490 00000-0 34558-3 0 9993
2 64569 97.7614 80.1002 0001142 13.0349 347.0899 14.92483898 23297Epoch: 2025-11-24T04:47Z
TLE epoch observation values (Epoch: 2025-11-24T04:47:12.018Z)
Latitude
-0.00008°
Longitude
-55.10271°
Altitude
592.46 km
Speed
7.564 km/s
True Right ascension
05h 20m 24s
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
12:29:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.007 km
Perigee altitude
586.416 km
Semi-major axis
6,965.348 km
Eccentricity
0.00011
Inclination
97.7614°
RAAN
80.1002°
Arg. of periapsis
13.0349°
True anomaly
347.08698°
Mean anomaly
347.0899°
Eccentric anomaly
347.08844°
Mean motion
3.73361 °/min
Orbital period
96.42 mins
BSTAR
0.00034558
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-24 19:50:14.910Z | 34.835° NE | 2025-11-24 19:54:14.910Z | 108.102° ESE | 26.293° | 2025-11-24 19:57:14.910Z | 157.187° SSE |
| 5 mins | 2025-11-24 21:27:14.910Z | 327.371° NNW | 2025-11-24 21:29:14.910Z | 290.625° WNW | 19.633° | 2025-11-24 21:32:14.910Z | 243.656° WSW |
| 4 mins | 2025-11-25 06:42:14.910Z | 92.802° ESE | 2025-11-25 06:43:14.910Z | 74.165° E | 18.744° | 2025-11-25 06:46:14.910Z | 23.972° NE |
| 6 mins | 2025-11-25 08:16:14.910Z | 208.283° SW | 2025-11-25 08:19:14.910Z | 273.973° WNW | 27.255° | 2025-11-25 08:22:14.910Z | 324.325° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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