IRIDE-MS2-HEO-6, 64576
Orbit data source: Space-Track
IRIDE-MS2-HEO-6, 64576 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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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: 6 hours ago
TLE from 6 hours ago
0 IRIDE-MS2-HEO-6
1 64576U 25135BA 26105.28510073 .00001120 00000-0 11072-3 0 9992
2 64576 97.7635 220.3286 0004138 149.8562 210.2897 14.93881703 44507Epoch: 2026-04-15T06:50Z
TLE epoch observation values (Epoch: 2026-04-15T06:50:32.703Z)
Latitude
0.00003°
Longitude
-85.75686°
Altitude
591.38 km
Speed
7.563 km/s
True Right ascension
14h 41m 18s
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
19:35:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.743 km
Perigee altitude
579.982 km
Semi-major axis
6,960.999 km
Eccentricity
0.00041
Inclination
97.7635°
RAAN
220.3286°
Arg. of periapsis
149.8562°
True anomaly
210.26579°
Mean anomaly
210.2897°
Eccentric anomaly
210.27775°
Mean motion
3.73711 °/min
Orbital period
96.33 mins
BSTAR
0.00011072
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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-6 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 | 2026-04-15 20:15:55.418Z | 20.754° NNE | 2026-04-15 20:19:55.418Z | 118.172° SE | 40.542° | 2026-04-15 20:22:55.418Z | 178.703° S |
| 6 mins | 2026-04-16 07:05:55.418Z | 129.832° SE | 2026-04-16 07:08:55.418Z | 60.037° ENE | 29.98° | 2026-04-16 07:11:55.418Z | 8.025° 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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