WREN-1, 60478
Orbit data source: Space-Track
WREN-1, 60478 is a payload satellite owned by C3S (HU) in SSO that was launched on Fri, 16 Aug 2024 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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60478 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
HU / HUNRelated business
Manufacturer
C3S
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.4 m
Radar Cross Section
0.115 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 WREN-1
1 60478U 24149L 25289.15166067 .00011556 00000-0 38349-3 0 9991
2 60478 97.3999 7.3403 0006554 66.1422 294.0506 15.31378876 64859Epoch: 2025-10-16T03:38Z
TLE epoch observation values (Epoch: 2025-10-16T03:38:23.481Z)
Latitude
-0.00001°
Longitude
-72.17303°
Altitude
472.976 km
Speed
7.63 km/s
True Right ascension
00h 29m 21s
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
12:35:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.135 km
Perigee altitude
464.16 km
Semi-major axis
6,846.785 km
Eccentricity
0.00066
Inclination
97.3999°
RAAN
7.3403°
Arg. of periapsis
66.1422°
True anomaly
293.98199°
Mean anomaly
294.0506°
Eccentric anomaly
294.0163°
Mean motion
3.83101 °/min
Orbital period
93.97 mins
BSTAR
0.00038349
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.WREN-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 | 2025-10-16 18:18:35.418Z | 7.027° NNE | 2025-10-16 18:21:35.418Z | 284.489° WNW | 43.665° | 2025-10-16 18:24:35.418Z | 199.917° SSW |
| 4 mins | 2025-10-17 04:53:35.418Z | 111.073° ESE | 2025-10-17 04:54:35.418Z | 79.401° E | 28.048° | 2025-10-17 04:57:35.418Z | 10.389° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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