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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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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 HERMES-1
1 63242U 25052AJ 26032.69167407 .00005467 00000-0 25612-3 0 9995
2 63242 97.4082 286.7555 0006016 309.0722 50.9977 15.20102507 49208Epoch: 2026-02-01T16:36Z
TLE epoch observation values (Epoch: 2026-02-01T16:36:00.639Z)
Latitude
-0.00008°
Longitude
-94.14483°
Altitude
506.016 km
Speed
7.613 km/s
True Right ascension
19h 07m 01s
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
07:16:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.636 km
Perigee altitude
498.358 km
Semi-major axis
6,880.634 km
Eccentricity
0.0006
Inclination
97.4082°
RAAN
286.7555°
Arg. of periapsis
309.0722°
True anomaly
51.0513°
Mean anomaly
50.9977°
Eccentric anomaly
51.0245°
Mean motion
3.80277 °/min
Orbital period
94.67 mins
BSTAR
0.00025612
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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
Did you know?
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 | 2026-02-02 05:47:45.431Z | 7.657° NNE | 2026-02-02 05:50:45.431Z | 325.232° NNW | 43.138° | 2026-02-02 05:53:45.431Z | 200.236° SSW |
| 5 mins | 2026-02-02 16:26:45.431Z | 130.936° SE | 2026-02-02 16:28:45.431Z | 74.5° E | 32.291° | 2026-02-02 16:31:45.431Z | 6.788° 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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