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: 11 hours ago
TLE from 11 hours ago
0 HERMES-1
1 63242U 25052AJ 26235.48658477 .00003977 00000-0 17656-3 0 9992
2 63242 97.3801 125.8827 0005876 320.6734 39.4075 15.22117376 80035Epoch: 2026-08-23T11:40Z
TLE epoch observation values (Epoch: 2026-08-23T11:40:40.924Z)
Latitude
0°
Longitude
-21.06976°
Altitude
499.427 km
Speed
7.616 km/s
True Right ascension
08h 23m 31s
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
14:02:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.456 km
Perigee altitude
492.377 km
Semi-major axis
6,874.554 km
Eccentricity
0.00059
Inclination
97.3801°
RAAN
125.8827°
Arg. of periapsis
320.6734°
True anomaly
39.45027°
Mean anomaly
39.4075°
Eccentric anomaly
39.42888°
Mean motion
3.80782 °/min
Orbital period
94.54 mins
BSTAR
0.00017656
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-24 05:35:40.670Z | 14.141° NNE | 2026-08-24 05:38:40.670Z | 77.411° E | 44.698° | 2026-08-24 05:41:40.670Z | 189.628° SSW |
| 5 mins | 2026-08-24 16:13:40.670Z | 120.634° SE | 2026-08-24 16:15:40.670Z | 72.643° E | 25.867° | 2026-08-24 16:18:40.670Z | 12.495° 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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