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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 HERMES-5
1 63834U 25052BQ 26129.68400030 .00007476 00000-0 27867-3 0 9996
2 63834 97.4011 24.3883 0002542 290.5432 69.5534 15.27727766 64073Epoch: 2026-05-09T16:24Z
TLE epoch observation values (Epoch: 2026-05-09T16:24:57.625Z)
Latitude
-0.00009°
Longitude
-89.3497°
Altitude
485.099 km
Speed
7.623 km/s
True Right ascension
01h 37m 33s
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
10:29:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.305 km
Perigee altitude
477.819 km
Semi-major axis
6,857.699 km
Eccentricity
0.00025
Inclination
97.4011°
RAAN
24.3883°
Arg. of periapsis
290.5432°
True anomaly
69.5807°
Mean anomaly
69.5534°
Eccentric anomaly
69.56705°
Mean motion
3.82187 °/min
Orbital period
94.19 mins
BSTAR
0.00027867
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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 | 2026-05-10 05:32:55.989Z | 23.052° NE | 2026-05-10 05:35:55.989Z | 79.269° E | 37.211° | 2026-05-10 05:38:55.989Z | 173.374° S |
| 4 mins | 2026-05-10 17:42:55.989Z | 230.967° WSW | 2026-05-10 17:43:55.989Z | 255.277° W | 22.038° | 2026-05-10 17:46:55.989Z | 317.577° NNW |
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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