UKUBE 1, 40074
Orbit data source: Space-Track
UKUBE 1, 40074 is a payload satellite owned by UKSA (UK) in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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40074 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
ClydeSpace
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.2 m
Radar Cross Section
0.038 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 UKUBE 1
1 40074U 14037F 26233.79599055 .00007056 00000-0 38808-3 0 9993
2 40074 98.4267 244.0175 0000939 36.0965 324.0327 15.14439558658483Epoch: 2026-08-21T19:06Z
TLE epoch observation values (Epoch: 2026-08-21T19:06:13.583Z)
Latitude
-0.00006°
Longitude
-12.6547°
Altitude
525.208 km
Speed
7.601 km/s
True Right ascension
16h 16m 04s
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
23:29:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.348 km
Perigee altitude
519.053 km
Semi-major axis
6,897.837 km
Eccentricity
0.00009
Inclination
98.4267°
RAAN
244.0175°
Arg. of periapsis
36.0965°
True anomaly
324.02638°
Mean anomaly
324.0327°
Eccentric anomaly
324.02954°
Mean motion
3.78856 °/min
Orbital period
95.02 mins
BSTAR
0.00038808
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Other satellites on launch #37 in the year 2014 (2014-07-08 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.UKUBE 1 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 | 2026-08-22 13:06:48.428Z | 36.065° NE | 2026-08-22 13:09:48.428Z | 92.303° ESE | 27.122° | 2026-08-22 13:12:48.428Z | 157.446° SSE |
| 4 mins | 2026-08-23 01:22:48.428Z | 222.686° SW | 2026-08-23 01:23:48.428Z | 247.927° W | 25.955° | 2026-08-23 01:26:48.428Z | 317.526° 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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