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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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, 0.7 m
Radar Cross Section
0.780 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 TYCHE
1 60496U 24149AE 26256.14330594 .00003059 00000-0 12219-3 0 9990
2 60496 97.3692 332.7390 0002248 42.6824 317.4589 15.25892091115312Epoch: 2026-09-13T03:26Z
TLE epoch observation values (Epoch: 2026-09-13T03:26:21.633Z)
Latitude
0.00002°
Longitude
-70.99333°
Altitude
490.07 km
Speed
7.621 km/s
True Right ascension
22h 10m 57s
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
09:57:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.607 km
Perigee altitude
483.522 km
Semi-major axis
6,863.201 km
Eccentricity
0.00022
Inclination
97.3692°
RAAN
332.739°
Arg. of periapsis
42.6824°
True anomaly
317.44148°
Mean anomaly
317.4589°
Eccentric anomaly
317.45019°
Mean motion
3.81727 °/min
Orbital period
94.31 mins
BSTAR
0.00012219
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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 | 2026-09-13 18:10:09.529Z | 7.309° NNE | 2026-09-13 18:13:09.529Z | 229.455° WSW | 67.677° | 2026-09-13 18:16:09.529Z | 198.068° SSW |
| 5 mins | 2026-09-14 04:46:09.529Z | 126.665° SE | 2026-09-14 04:48:09.529Z | 73.028° E | 34.254° | 2026-09-14 04:51:09.529Z | 8.902° NNE |
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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