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: 10 hours ago
TLE from 10 hours ago
0 IRIDE-MS2-HEO-3
1 64568U 25135AS 26133.20614291 .00000621 00000-0 66980-4 0 9997
2 64568 97.7692 247.8416 0002186 76.8558 283.2905 14.91890213 48660Epoch: 2026-05-13T04:56Z
TLE epoch observation values (Epoch: 2026-05-13T04:56:50.747Z)
Latitude
0.00002°
Longitude
-57.33934°
Altitude
594.734 km
Speed
7.563 km/s
True Right ascension
16h 31m 21s
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
22:53:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.584 km
Perigee altitude
587.538 km
Semi-major axis
6,967.198 km
Eccentricity
0.00022
Inclination
97.7692°
RAAN
247.8416°
Arg. of periapsis
76.8558°
True anomaly
283.26612°
Mean anomaly
283.2905°
Eccentric anomaly
283.27831°
Mean motion
3.73212 °/min
Orbital period
96.46 mins
BSTAR
0.00006698
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-13 20:00:25.618Z | 31.899° NE | 2026-05-13 20:03:25.618Z | 85.053° E | 31.425° | 2026-05-13 20:07:25.618Z | 166.314° S |
| 4 mins | 2026-05-13 21:37:25.618Z | 320.59° NNW | 2026-05-13 21:39:25.618Z | 286.501° WNW | 16.032° | 2026-05-13 21:41:25.618Z | 256.407° W |
| 5 mins | 2026-05-14 06:51:25.618Z | 112.536° SE | 2026-05-14 06:53:25.618Z | 74.813° E | 22.821° | 2026-05-14 06:56:25.618Z | 19.705° NNE |
| 5 mins | 2026-05-14 08:27:25.618Z | 228.723° WSW | 2026-05-14 08:29:25.618Z | 271.578° WNW | 22.598° | 2026-05-14 08:32:25.618Z | 319.346° 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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