IRIDE-MS2-HEO-3, 64568
Orbit data source: Space-Track
IRIDE-MS2-HEO-3, 64568 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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64568 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: 4 hours ago
TLE from 4 hours ago
0 IRIDE-MS2-HEO-3
1 64568U 25135AS 25328.53168159 .00003411 00000-0 33628-3 0 9997
2 64568 97.7592 80.3969 0001121 266.0874 94.0217 14.92678524 23346Epoch: 2025-11-24T12:45Z
TLE epoch observation values (Epoch: 2025-11-24T12:45:37.289Z)
Latitude
-0.00003°
Longitude
-174.73878°
Altitude
592.686 km
Speed
7.564 km/s
True Right ascension
05h 21m 35s
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
14:18:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.386 km
Perigee altitude
585.825 km
Semi-major axis
6,964.742 km
Eccentricity
0.00011
Inclination
97.7592°
RAAN
80.3969°
Arg. of periapsis
266.0874°
True anomaly
94.03451°
Mean anomaly
94.0217°
Eccentric anomaly
94.02811°
Mean motion
3.7341 °/min
Orbital period
96.41 mins
BSTAR
0.00033628
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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-3 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 | 2025-11-24 19:46:18.049Z | 39.629° NE | 2025-11-24 19:49:18.049Z | 90.047° ESE | 24.388° | 2025-11-24 19:52:18.049Z | 148.142° SSE |
| 4 mins | 2025-11-24 21:23:18.049Z | 323.768° NNW | 2025-11-24 21:25:18.049Z | 282.562° WNW | 21.08° | 2025-11-24 21:27:18.049Z | 247.989° W |
| 5 mins | 2025-11-25 08:12:18.049Z | 209.774° SW | 2025-11-25 08:14:18.049Z | 256.681° W | 29.964° | 2025-11-25 08:17:18.049Z | 322.161° 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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