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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 HERMES-5
1 63834U 25052BQ 26254.68069771 .00004940 00000-0 17240-3 0 9995
2 63834 97.3846 148.5924 0003646 172.9693 187.1600 15.30064003 83176Epoch: 2026-09-11T16:20Z
TLE epoch observation values (Epoch: 2026-09-11T16:20:12.282Z)
Latitude
0.00006°
Longitude
-87.15935°
Altitude
481.206 km
Speed
7.624 km/s
True Right ascension
09h 54m 22s
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
09:30:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.07 km
Perigee altitude
470.075 km
Semi-major axis
6,850.71 km
Eccentricity
0.00036
Inclination
97.3846°
RAAN
148.5924°
Arg. of periapsis
172.9693°
True anomaly
187.15479°
Mean anomaly
187.16°
Eccentric anomaly
187.1574°
Mean motion
3.82772 °/min
Orbital period
94.05 mins
BSTAR
0.0001724
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-12 17:34:25.128Z | 199.397° SSW | 2026-09-12 17:37:25.128Z | 269.766° W | 33.115° | 2026-09-12 17:40:25.128Z | 328.257° NNW |
| 4 mins | 2026-09-13 06:34:25.128Z | 334.546° NNW | 2026-09-13 06:36:25.128Z | 287.667° WNW | 25.545° | 2026-09-13 06:38:25.128Z | 241.972° WSW |
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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