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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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: 5 hours ago
TLE from 5 hours ago
0 IRIDE-MS2-HEO-3
1 64568U 25135AS 26132.20008579 .00000460 00000-0 51030-4 0 9993
2 64568 97.7690 246.8498 0002230 78.2907 281.8562 14.91887496 48517Epoch: 2026-05-12T04:48Z
TLE epoch observation values (Epoch: 2026-05-12T04:48:07.412Z)
Latitude
-0°
Longitude
-55.15896°
Altitude
594.773 km
Speed
7.563 km/s
True Right ascension
16h 27m 23s
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
18:19:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.623 km
Perigee altitude
587.516 km
Semi-major axis
6,967.207 km
Eccentricity
0.00022
Inclination
97.769°
RAAN
246.8498°
Arg. of periapsis
78.2907°
True anomaly
281.83119°
Mean anomaly
281.8562°
Eccentric anomaly
281.8437°
Mean motion
3.73212 °/min
Orbital period
96.46 mins
BSTAR
0.00005103
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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 | 2026-05-12 19:52:18.611Z | 41.21° NE | 2026-05-12 19:55:18.611Z | 102.308° ESE | 26.92° | 2026-05-12 19:58:18.611Z | 155.934° SSE |
| 4 mins | 2026-05-12 21:29:18.611Z | 315.226° NNW | 2026-05-12 21:30:18.611Z | 295.767° NW | 19.384° | 2026-05-12 21:33:18.611Z | 246.411° WSW |
| 4 mins | 2026-05-13 06:43:18.611Z | 100.646° ESE | 2026-05-13 06:45:18.611Z | 63.486° ENE | 19.214° | 2026-05-13 06:47:18.611Z | 29.196° NE |
| 5 mins | 2026-05-13 08:18:18.611Z | 214.901° SW | 2026-05-13 08:20:18.611Z | 258.724° W | 27.118° | 2026-05-13 08:23:18.611Z | 319.358° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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