TYCHE, 60496
Orbit data source: Space-Track
TYCHE, 60496 is a UK payload satellite 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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60496 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL
Mission
Operational Commercial Imaging
Bus & Motor
CARBONITE+, Unknown motor
Mass
150 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.780 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 TYCHE
1 60496U 24149AE 25297.78184435 .00007406 00000-0 29831-3 0 9993
2 60496 97.3994 13.4457 0005351 57.5736 302.6019 15.25134209 66004Epoch: 2025-10-24T18:45Z
TLE epoch observation values (Epoch: 2025-10-24T18:45:51.351Z)
Latitude
-0.00003°
Longitude
58.55993°
Altitude
491.501 km
Speed
7.62 km/s
True Right ascension
00h 53m 46s
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
23:01:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.015 km
Perigee altitude
483.667 km
Semi-major axis
6,865.478 km
Eccentricity
0.00054
Inclination
97.3994°
RAAN
13.4457°
Arg. of periapsis
57.5736°
True anomaly
302.55023°
Mean anomaly
302.6019°
Eccentric anomaly
302.57606°
Mean motion
3.81537 °/min
Orbital period
94.36 mins
BSTAR
0.00029831
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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.TYCHE 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 | 2025-10-25 04:22:11.348Z | 105.368° ESE | 2025-10-25 04:24:11.348Z | 64.999° ENE | 17.832° | 2025-10-25 04:26:11.348Z | 27.847° NE |
| 4 mins | 2025-10-25 05:56:11.348Z | 233.376° WSW | 2025-10-25 05:57:11.348Z | 258.042° W | 21.959° | 2025-10-25 06:00:11.348Z | 318.198° NNW |
| 4 mins | 2025-10-25 17:24:11.348Z | 63.042° ENE | 2025-10-25 17:25:11.348Z | 88.004° E | 22.903° | 2025-10-25 17:28:11.348Z | 150.715° SSE |
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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