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: 10 hours ago
TLE from 10 hours ago
0 TYCHE
1 60496U 24149AE 25260.90125770 .00005252 00000-0 21655-3 0 9997
2 60496 97.4038 336.9982 0004882 156.4238 203.7224 15.24488447 60383Epoch: 2025-09-17T21:37Z
TLE epoch observation values (Epoch: 2025-09-17T21:37:48.665Z)
Latitude
-0.00003°
Longitude
15.47487°
Altitude
498.49 km
Speed
7.614 km/s
True Right ascension
22h 27m 59s
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
00:11:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.634 km
Perigee altitude
485.929 km
Semi-major axis
6,867.419 km
Eccentricity
0.00049
Inclination
97.4038°
RAAN
336.9982°
Arg. of periapsis
156.4238°
True anomaly
203.69991°
Mean anomaly
203.7224°
Eccentric anomaly
203.71115°
Mean motion
3.81376 °/min
Orbital period
94.4 mins
BSTAR
0.00021655
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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 | 2025-09-18 17:07:13.134Z | 59.669° ENE | 2025-09-18 17:09:13.134Z | 96.811° ESE | 15.557° | 2025-09-18 17:11:13.134Z | 131.892° SE |
| 4 mins | 2025-09-18 18:41:13.134Z | 327.281° NNW | 2025-09-18 18:42:13.134Z | 302.787° NW | 24.148° | 2025-09-18 18:45:13.134Z | 234.236° WSW |
| 6 mins | 2025-09-19 05:16:13.134Z | 171.523° S | 2025-09-19 05:18:13.134Z | 187.276° SSW | 42.068° | 2025-09-19 05:22:13.134Z | 345.99° N |
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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