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: 1 day ago
TLE from 1 day ago
0 TYCHE
1 60496U 24149AE 25315.16700559 .00008293 00000-0 33101-3 0 9997
2 60496 97.3977 30.6314 0003984 5.2079 354.9199 15.25407398 68652Epoch: 2025-11-11T04:00Z
TLE epoch observation values (Epoch: 2025-11-11T04:00:29.282Z)
Latitude
-0.00014°
Longitude
-80.04804°
Altitude
489.934 km
Speed
7.622 km/s
True Right ascension
02h 02m 31s
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
06:21:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.256 km
Perigee altitude
483.786 km
Semi-major axis
6,864.658 km
Eccentricity
0.0004
Inclination
97.3977°
RAAN
30.6314°
Arg. of periapsis
5.2079°
True anomaly
354.91586°
Mean anomaly
354.9199°
Eccentric anomaly
354.91788°
Mean motion
3.81606 °/min
Orbital period
94.34 mins
BSTAR
0.00033101
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-12 18:20:45.304Z | 359.408° N | 2025-11-12 18:23:45.304Z | 296.865° NW | 36.938° | 2025-11-12 18:26:45.304Z | 213.179° SW |
| 5 mins | 2025-11-13 04:57:45.304Z | 140.099° SSE | 2025-11-13 04:59:45.304Z | 57.35° ENE | 37.802° | 2025-11-13 05:02:45.304Z | 359.093° N |
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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