HERMES-6, 63489
Orbit data source: Space-Track
HERMES-6, 63489 is a payload satellite owned by ASI (IT) in SSO that was launched on Sat, 15 Mar 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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63489 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
MILANP/INAFI
Mission
Operational Civil Astronomy
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 HERMES-6
1 63489U 25052BK 25287.17359431 .00008287 00000-0 40096-3 0 9998
2 63489 97.4185 178.5879 0005692 326.5080 33.5794 15.18824112 32433Epoch: 2025-10-14T04:09Z
TLE epoch observation values (Epoch: 2025-10-14T04:09:58.548Z)
Latitude
0°
Longitude
93.12813°
Altitude
509.215 km
Speed
7.611 km/s
True Right ascension
11h 54m 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
15:54:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.28 km
Perigee altitude
502.443 km
Semi-major axis
6,884.498 km
Eccentricity
0.00057
Inclination
97.4185°
RAAN
178.5879°
Arg. of periapsis
326.508°
True anomaly
33.6155°
Mean anomaly
33.5794°
Eccentric anomaly
33.59745°
Mean motion
3.79957 °/min
Orbital period
94.75 mins
BSTAR
0.00040096
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.HERMES-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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-15 06:01:33.649Z | 359.276° N | 2025-10-15 06:04:33.649Z | 279.714° WNW | 38.673° | 2025-10-15 06:07:33.649Z | 210.241° SW |
| 5 mins | 2025-10-15 16:40:33.649Z | 146.028° SSE | 2025-10-15 16:42:33.649Z | 89.424° E | 39.172° | 2025-10-15 16:45:33.649Z | 0.275° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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