HERMES-1, 63242
Orbit data source: Space-Track
HERMES-1, 63242 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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63242 intel report (Beta)
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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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 HERMES-1
1 63242U 25052AJ 26175.19410603 .00004072 00000-0 18316-3 0 9991
2 63242 97.3900 66.6900 0008133 147.5973 212.5764 15.21641059 70867Epoch: 2026-06-24T04:39Z
TLE epoch observation values (Epoch: 2026-06-24T04:39:30.760Z)
Latitude
-0.00005°
Longitude
84.45702°
Altitude
508.7 km
Speed
7.607 km/s
True Right ascension
04h 26m 45s
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
21:55:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.445 km
Perigee altitude
492.261 km
Semi-major axis
6,875.99 km
Eccentricity
0.00081
Inclination
97.39°
RAAN
66.69°
Arg. of periapsis
147.5973°
True anomaly
212.52626°
Mean anomaly
212.5764°
Eccentric anomaly
212.55133°
Mean motion
3.80663 °/min
Orbital period
94.57 mins
BSTAR
0.00018316
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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-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-24 15:51:39.605Z | 105.511° ESE | 2026-06-24 15:53:39.605Z | 71.636° E | 15.431° | 2026-06-24 15:55:39.605Z | 35.29° NE |
| 4 mins | 2026-06-24 17:25:39.605Z | 217.75° SW | 2026-06-24 17:27:39.605Z | 272.882° WNW | 26.439° | 2026-06-24 17:29:39.605Z | 316.843° NNW |
| 4 mins | 2026-06-25 04:55:39.605Z | 64.6° ENE | 2026-06-25 04:56:39.605Z | 86.891° E | 20.161° | 2026-06-25 04:59:39.605Z | 145.579° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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