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 26287.30303881 .00006671 00000-0 36073-3 0 9993
2 40074 98.4245 303.2610 0002886 108.9977 251.1566 15.15070012666588Epoch: 2026-10-14T07:16Z
TLE epoch observation values (Epoch: 2026-10-14T07:16:22.553Z)
Latitude
0.00007°
Longitude
171.31232°
Altitude
524.462 km
Speed
7.601 km/s
True Right ascension
20h 13m 02s
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
14:45:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.775 km
Perigee altitude
515.795 km
Semi-major axis
6,895.922 km
Eccentricity
0.00029
Inclination
98.4245°
RAAN
303.261°
Arg. of periapsis
108.9977°
True anomaly
251.1253°
Mean anomaly
251.1566°
Eccentric anomaly
251.14095°
Mean motion
3.79013 °/min
Orbital period
94.98 mins
BSTAR
0.00036073
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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 | 2026-10-15 00:50:13.178Z | 145.128° SSE | 2026-10-15 00:53:13.178Z | 84.258° E | 46.862° | 2026-10-15 00:56:13.178Z | 3.035° NNE |
| 5 mins | 2026-10-15 13:58:13.178Z | 25.924° NE | 2026-10-15 14:00:13.178Z | 92.404° ESE | 64.521° | 2026-10-15 14:03:13.178Z | 182.342° SSW |
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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