HERMES-5, 63834
Orbit data source: Space-Track
HERMES-5, 63834 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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63834 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, 0.2 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 HERMES-5
1 63834U 25052BQ 25298.64924179 .00013310 00000-0 59650-3 0 9992
2 63834 97.4202 190.3922 0003185 245.4521 114.6382 15.21355104 34207Epoch: 2025-10-25T15:34Z
TLE epoch observation values (Epoch: 2025-10-25T15:34:54.490Z)
Latitude
-0.00014°
Longitude
-77.61158°
Altitude
505.758 km
Speed
7.611 km/s
True Right ascension
12h 41m 34s
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
23:08:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.907 km
Perigee altitude
496.527 km
Semi-major axis
6,876.854 km
Eccentricity
0.00032
Inclination
97.4202°
RAAN
190.3922°
Arg. of periapsis
245.4521°
True anomaly
114.67137°
Mean anomaly
114.6382°
Eccentric anomaly
114.65479°
Mean motion
3.80591 °/min
Orbital period
94.59 mins
BSTAR
0.0005965
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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-5 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 | 2025-10-26 04:47:47.223Z | 59.296° ENE | 2025-10-26 04:49:47.223Z | 93.647° ESE | 14.437° | 2025-10-26 04:51:47.223Z | 127.648° SE |
| 5 mins | 2025-10-26 06:21:47.223Z | 335.847° NNW | 2025-10-26 06:23:47.223Z | 281.723° WNW | 27.373° | 2025-10-26 06:26:47.223Z | 225.297° WSW |
| 5 mins | 2025-10-26 16:58:47.223Z | 168.526° S | 2025-10-26 17:00:47.223Z | 194.796° SSW | 44.888° | 2025-10-26 17:03:47.223Z | 347.27° 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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