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: 14 hours ago
TLE from 14 hours ago
0 IRIDE-MS2-HEO-3
1 64568U 25135AS 26207.58609155 .00002071 00000-0 21003-3 0 9990
2 64568 97.7764 321.2002 0001850 129.0937 231.0447 14.91965995 59751Epoch: 2026-07-26T14:03Z
TLE epoch observation values (Epoch: 2026-07-26T14:03:58.309Z)
Latitude
-0.00001°
Longitude
165.92535°
Altitude
595.658 km
Speed
7.562 km/s
True Right ascension
21h 24m 48s
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
17:27:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.114 km
Perigee altitude
587.536 km
Semi-major axis
6,966.962 km
Eccentricity
0.00019
Inclination
97.7764°
RAAN
321.2002°
Arg. of periapsis
129.0937°
True anomaly
231.02822°
Mean anomaly
231.0447°
Eccentric anomaly
231.03646°
Mean motion
3.73231 °/min
Orbital period
96.45 mins
BSTAR
0.00021003
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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 | 2026-07-27 07:54:05.108Z | 183.513° SSW | 2026-07-27 07:57:05.108Z | 269.435° W | 40.6° | 2026-07-27 08:00:05.108Z | 336.502° NNW |
| 5 mins | 2026-07-27 19:38:05.108Z | 56.468° ENE | 2026-07-27 19:40:05.108Z | 92.184° ESE | 19.656° | 2026-07-27 19:43:05.108Z | 141.751° SSE |
| 5 mins | 2026-07-27 21:14:05.108Z | 328.807° NNW | 2026-07-27 21:16:05.108Z | 280.296° WNW | 25.866° | 2026-07-27 21:19:05.108Z | 231.159° 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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