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: 15 hours ago
TLE from 15 hours ago
0 UKUBE 1
1 40074U 14037F 26303.87901429 .00005108 00000-0 27574-3 0 9996
2 40074 98.4231 321.6185 0002867 81.5597 278.5958 15.15266395669095Epoch: 2026-10-30T21:05Z
TLE epoch observation values (Epoch: 2026-10-30T21:05:46.834Z)
Latitude
0.00003°
Longitude
-34.01941°
Altitude
522.928 km
Speed
7.602 km/s
True Right ascension
21h 26m 28s
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
08:03:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.165 km
Perigee altitude
515.212 km
Semi-major axis
6,895.325 km
Eccentricity
0.00029
Inclination
98.4231°
RAAN
321.6185°
Arg. of periapsis
81.5597°
True anomaly
278.56331°
Mean anomaly
278.5958°
Eccentric anomaly
278.57956°
Mean motion
3.79063 °/min
Orbital period
94.97 mins
BSTAR
0.00027574
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-31 13:31:41.457Z | 51.028° ENE | 2026-10-31 13:33:41.457Z | 90.315° ESE | 23.421° | 2026-10-31 13:36:41.457Z | 148.353° SSE |
| 4 mins | 2026-10-31 15:06:41.457Z | 318.221° NNW | 2026-10-31 15:07:41.457Z | 296.036° NW | 21.836° | 2026-10-31 15:10:41.457Z | 241.656° WSW |
| 5 mins | 2026-11-01 01:45:41.457Z | 200.72° SSW | 2026-11-01 01:47:41.457Z | 255.978° W | 40.733° | 2026-11-01 01:50:41.457Z | 327.512° NNW |
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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