HERMES-2, 63243
Orbit data source: Space-Track
HERMES-2, 63243 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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63243 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, 0.2 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 HERMES-2
1 63243U 25052AK 26061.59363737 .00010252 00000-0 37924-3 0 9998
2 63243 97.4027 317.2091 0006058 117.6562 242.5293 15.27864816 53732Epoch: 2026-03-02T14:14Z
TLE epoch observation values (Epoch: 2026-03-02T14:14:50.268Z)
Latitude
-0.00003°
Longitude
-56.88516°
Altitude
487.217 km
Speed
7.62 km/s
True Right ascension
21h 08m 50s
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
00:42:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.306 km
Perigee altitude
474.997 km
Semi-major axis
6,857.289 km
Eccentricity
0.00061
Inclination
97.4027°
RAAN
317.2091°
Arg. of periapsis
117.6562°
True anomaly
242.46773°
Mean anomaly
242.5293°
Eccentric anomaly
242.49851°
Mean motion
3.82221 °/min
Orbital period
94.19 mins
BSTAR
0.00037924
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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-2 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 | 2026-03-03 04:58:31.795Z | 55.885° ENE | 2026-03-03 05:00:31.795Z | 93.992° ESE | 16.825° | 2026-03-03 05:02:31.795Z | 132.299° SE |
| 4 mins | 2026-03-03 06:32:31.795Z | 323.784° NNW | 2026-03-03 06:33:31.795Z | 299.822° NW | 22.087° | 2026-03-03 06:36:31.795Z | 236.291° WSW |
| 5 mins | 2026-03-03 17:06:31.795Z | 175.857° S | 2026-03-03 17:08:31.795Z | 251.2° W | 43.997° | 2026-03-03 17:11:31.795Z | 343.636° N |
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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