IRIDE-MS2-HEO-2, 64569
Orbit data source: Space-Track
IRIDE-MS2-HEO-2, 64569 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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64569 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-2
1 64569U 25135AT 26260.29890803 .00001216 00000-0 11966-3 0 9997
2 64569 97.7829 13.6540 0002874 68.5379 291.6147 14.93937921 67632Epoch: 2026-09-17T07:10Z
TLE epoch observation values (Epoch: 2026-09-17T07:10:25.653Z)
Latitude
-0.00006°
Longitude
-90.19103°
Altitude
587.978 km
Speed
7.567 km/s
True Right ascension
00h 54m 36s
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
05:02:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.689 km
Perigee altitude
580.688 km
Semi-major axis
6,960.825 km
Eccentricity
0.00029
Inclination
97.7829°
RAAN
13.654°
Arg. of periapsis
68.5379°
True anomaly
291.58408°
Mean anomaly
291.6147°
Eccentric anomaly
291.59939°
Mean motion
3.73725 °/min
Orbital period
96.33 mins
BSTAR
0.00011966
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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-2 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 | 2026-09-17 20:35:49.229Z | 10.429° NNE | 2026-09-17 20:39:49.229Z | 212.585° SW | 69.54° | 2026-09-17 20:42:49.229Z | 196.554° SSW |
| 6 mins | 2026-09-18 07:25:49.229Z | 145.202° SSE | 2026-09-18 07:27:49.229Z | 95.054° ESE | 56.056° | 2026-09-18 07:31:49.229Z | 356.951° N |
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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