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: 8 hours ago
TLE from 8 hours ago
0 IRIDE-MS2-HEO-3
1 64568U 25135AS 26036.25167353 .00004777 00000-0 46228-3 0 9994
2 64568 97.7588 152.1157 0003173 52.0579 308.0927 14.93217836 34199Epoch: 2026-02-05T06:02Z
TLE epoch observation values (Epoch: 2026-02-05T06:02:24.592Z)
Latitude
-0.00005°
Longitude
-73.89334°
Altitude
589.59 km
Speed
7.566 km/s
True Right ascension
10h 08m 27s
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
15:58:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.136 km
Perigee altitude
582.717 km
Semi-major axis
6,963.064 km
Eccentricity
0.00032
Inclination
97.7588°
RAAN
152.1157°
Arg. of periapsis
52.0579°
True anomaly
308.06408°
Mean anomaly
308.0927°
Eccentric anomaly
308.07839°
Mean motion
3.73545 °/min
Orbital period
96.37 mins
BSTAR
0.00046228
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-05 19:30:06.565Z | 58.874° ENE | 2026-02-05 19:32:06.565Z | 91.598° ESE | 16.698° | 2026-02-05 19:34:06.565Z | 125.325° SE |
| 6 mins | 2026-02-05 21:05:06.565Z | 345.882° N | 2026-02-05 21:08:06.565Z | 277.24° WNW | 29.439° | 2026-02-05 21:11:06.565Z | 225.546° WSW |
| 6 mins | 2026-02-06 07:54:06.565Z | 184.502° SSW | 2026-02-06 07:57:06.565Z | 270.89° WNW | 40.079° | 2026-02-06 08:00:06.565Z | 336.117° NNW |
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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