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: 7 hours ago
TLE from 7 hours ago
0 IRIDE-MS2-HEO-2
1 64569U 25135AT 26133.29087876 .00000879 00000-0 88873-4 0 9990
2 64569 97.7710 247.9686 0003143 103.8648 256.2921 14.93521498 48674Epoch: 2026-05-13T06:58Z
TLE epoch observation values (Epoch: 2026-05-13T06:58:51.924Z)
Latitude
-0.0001°
Longitude
-87.80075°
Altitude
590.529 km
Speed
7.565 km/s
True Right ascension
16h 31m 52s
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
22:52:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.171 km
Perigee altitude
581.795 km
Semi-major axis
6,962.12 km
Eccentricity
0.00031
Inclination
97.771°
RAAN
247.9686°
Arg. of periapsis
103.8648°
True anomaly
256.25711°
Mean anomaly
256.2921°
Eccentric anomaly
256.27461°
Mean motion
3.73621 °/min
Orbital period
96.35 mins
BSTAR
0.000088873
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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 | 2026-05-13 20:24:22.264Z | 16.028° NNE | 2026-05-13 20:28:22.264Z | 141.414° SSE | 43.645° | 2026-05-13 20:31:22.264Z | 187.146° SSW |
| 6 mins | 2026-05-14 07:14:22.264Z | 138.672° SSE | 2026-05-14 07:17:22.264Z | 61.477° ENE | 34.894° | 2026-05-14 07:20:22.264Z | 4.018° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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