HOTSAT-2, 68465
Orbit data source: Space-Track
HOTSAT-2, 68465 is a payload satellite owned by Satellite Vu (UK) in SSO that was launched on Mon, 30 Mar 2026 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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68465 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
SSTL
Mission
Operational spacecraft
Bus & Motor
DARKCARB, H2O AOCS
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.9 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 HOTSAT-2
1 68465U 26067BB 26171.40614882 .00002421 00000-0 12394-3 0 9991
2 68465 97.4528 129.7219 0005066 72.2720 287.9066 15.17555908 12427Epoch: 2026-06-20T09:44Z
TLE epoch observation values (Epoch: 2026-06-20T09:44:51.258Z)
Latitude
-0.00003°
Longitude
74.8871°
Altitude
515.244 km
Speed
7.607 km/s
True Right ascension
08h 38m 53s
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
15:15:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.691 km
Perigee altitude
506.711 km
Semi-major axis
6,888.338 km
Eccentricity
0.00051
Inclination
97.4528°
RAAN
129.7219°
Arg. of periapsis
72.272°
True anomaly
287.85135°
Mean anomaly
287.9066°
Eccentric anomaly
287.87898°
Mean motion
3.7964 °/min
Orbital period
94.83 mins
BSTAR
0.00012394
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.HOTSAT-2 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 | 2026-06-22 09:47:07.440Z | 25.711° NE | 2026-06-22 09:50:07.440Z | 88.709° E | 36.41° | 2026-06-22 09:53:07.440Z | 170.977° S |
| 4 mins | 2026-06-22 22:02:07.440Z | 238.067° WSW | 2026-06-22 22:03:07.440Z | 262.791° W | 22.042° | 2026-06-22 22:06:07.440Z | 318.781° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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