IRIDE-MS2-HEO-9, 64585
Orbit data source: Space-Track
IRIDE-MS2-HEO-9, 64585 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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64585 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: 17 hours ago
TLE from 17 hours ago
0 IRIDE-MS2-HEO-9
1 64585U 25135BK 26224.56432484 .00000516 00000-0 56389-4 0 9993
2 64585 97.7803 338.3593 0002532 129.4399 230.7044 14.92011510 62302Epoch: 2026-08-12T13:32Z
TLE epoch observation values (Epoch: 2026-08-12T13:32:37.666Z)
Latitude
-0.00003°
Longitude
174.18591°
Altitude
595.824 km
Speed
7.561 km/s
True Right ascension
22h 33m 26s
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
21:05:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.448 km
Perigee altitude
586.92 km
Semi-major axis
6,966.821 km
Eccentricity
0.00025
Inclination
97.7803°
RAAN
338.3593°
Arg. of periapsis
129.4399°
True anomaly
230.68195°
Mean anomaly
230.7044°
Eccentric anomaly
230.69317°
Mean motion
3.73243 °/min
Orbital period
96.45 mins
BSTAR
0.000056389
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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-9 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 | 2026-08-13 07:22:09.652Z | 150.797° SSE | 2026-08-13 07:26:09.652Z | 61.393° ENE | 39.125° | 2026-08-13 07:29:09.652Z | 359.874° N |
| 6 mins | 2026-08-13 20:42:09.652Z | 4.741° NNE | 2026-08-13 20:45:09.652Z | 248.086° W | 42.603° | 2026-08-13 20:48:09.652Z | 202.33° SSW |
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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