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 Commercial 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: 21 hours ago
TLE from 21 hours ago
0 UKUBE 1
1 40074U 14037F 26205.44803441 .00010335 00000-0 57201-3 0 9993
2 40074 98.4250 212.6519 0002913 72.3459 287.8088 15.14069415654198Epoch: 2026-07-24T10:45Z
TLE epoch observation values (Epoch: 2026-07-24T10:45:10.173Z)
Latitude
0.00003°
Longitude
109.18498°
Altitude
526.242 km
Speed
7.6 km/s
True Right ascension
14h 10m 36s
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
20:31:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
522.835 km
Perigee altitude
518.816 km
Semi-major axis
6,898.962 km
Eccentricity
0.00029
Inclination
98.425°
RAAN
212.6519°
Arg. of periapsis
72.3459°
True anomaly
287.77702°
Mean anomaly
287.8088°
Eccentric anomaly
287.79291°
Mean motion
3.78763 °/min
Orbital period
95.05 mins
BSTAR
0.00057201
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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 | 2026-07-25 12:42:20.885Z | 45.891° ENE | 2026-07-25 12:45:20.885Z | 103.063° ESE | 21.018° | 2026-07-25 12:47:20.885Z | 141.59° SSE |
| 4 mins | 2026-07-25 14:17:20.885Z | 328.849° NNW | 2026-07-25 14:19:20.885Z | 285.469° WNW | 20.88° | 2026-07-25 14:21:20.885Z | 247.282° WSW |
| 5 mins | 2026-07-26 00:57:20.885Z | 198.866° SSW | 2026-07-26 00:59:20.885Z | 251.088° W | 33.309° | 2026-07-26 01:02:20.885Z | 327.095° 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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