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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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 26081.18577133 .00024909 00000-0 66675-3 0 9994
2 60478 97.3787 164.6063 0004442 198.6705 161.4378 15.38013652 88936Epoch: 2026-03-22T04:27Z
TLE epoch observation values (Epoch: 2026-03-22T04:27:30.642Z)
Latitude
-0.00002°
Longitude
-81.96713°
Altitude
457.976 km
Speed
7.636 km/s
True Right ascension
10h 58m 25s
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
23:37:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.957 km
Perigee altitude
445.892 km
Semi-major axis
6,827.061 km
Eccentricity
0.00044
Inclination
97.3787°
RAAN
164.6063°
Arg. of periapsis
198.6705°
True anomaly
161.454°
Mean anomaly
161.4378°
Eccentric anomaly
161.4459°
Mean motion
3.84762 °/min
Orbital period
93.56 mins
BSTAR
0.00066675
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-22 19:04:39.373Z | 331.417° NNW | 2026-03-22 19:06:39.373Z | 283.727° WNW | 21.152° | 2026-03-22 19:08:39.373Z | 241.42° WSW |
| 5 mins | 2026-03-23 05:34:39.373Z | 169.376° S | 2026-03-23 05:36:39.373Z | 182.499° SSW | 43.712° | 2026-03-23 05:39:39.373Z | 346.682° N |
| 4 mins | 2026-03-23 18:30:39.373Z | 0.795° NNE | 2026-03-23 18:32:39.373Z | 232.246° WSW | 40.871° | 2026-03-23 18:34:39.373Z | 201.993° SSW |
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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