FUNCUBE 1, 39444
Orbit data source: Space-Track
FUNCUBE 1, 39444 is a UK payload satellite in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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39444 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
ISIS BV
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FUNCUBE 1
1 39444U 13066AE 25300.39267293 .00010984 00000-0 76896-3 0 9992
2 39444 97.7991 263.1577 0037875 274.8147 84.8755 15.04843623644593Epoch: 2025-10-27T09:25Z
TLE epoch observation values (Epoch: 2025-10-27T09:25:26.941Z)
Latitude
0.00005°
Longitude
85.80027°
Altitude
552.798 km
Speed
7.587 km/s
True Right ascension
17h 32m 37s
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
15:44:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.225 km
Perigee altitude
522.752 km
Semi-major axis
6,927.126 km
Eccentricity
0.00379
Inclination
97.7991°
RAAN
263.1577°
Arg. of periapsis
274.8147°
True anomaly
85.30796°
Mean anomaly
84.8755°
Eccentric anomaly
85.09171°
Mean motion
3.76455 °/min
Orbital period
95.63 mins
BSTAR
0.00076896
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Other satellites on launch #66 in the year 2013 (2013-11-21 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.FUNCUBE 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 | 2025-10-27 20:45:05.909Z | 106.833° ESE | 2025-10-27 20:47:05.909Z | 71.868° E | 18.98° | 2025-10-27 20:50:05.909Z | 21.819° NNE |
| 5 mins | 2025-10-27 22:20:05.909Z | 221.248° SW | 2025-10-27 22:22:05.909Z | 270.859° WNW | 26.152° | 2025-10-27 22:25:05.909Z | 322.968° NNW |
| 5 mins | 2025-10-28 09:57:05.909Z | 45.988° ENE | 2025-10-28 09:59:05.909Z | 89.864° E | 27.752° | 2025-10-28 10:02:05.909Z | 154.634° SSE |
| 4 mins | 2025-10-28 11:32:05.909Z | 324.147° NNW | 2025-10-28 11:34:05.909Z | 287.47° WNW | 17.907° | 2025-10-28 11:36:05.909Z | 254.107° W |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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