ICUBE 1, 39432
Orbit data source: Space-Track
ICUBE 1, 39432 is a payload satellite owned by IST (PK) 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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39432 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / PAKIRelated business
Manufacturer
IST
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1.08 kg wet, 1.08 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: 8 hours ago
TLE from 8 hours ago
0 ICUBE 1
1 39432U 13066S 25300.50714782 .00015957 00000-0 77685-3 0 9994
2 39432 97.5517 279.8270 0022017 67.5187 292.8375 15.18241441649015Epoch: 2025-10-27T12:10Z
TLE epoch observation values (Epoch: 2025-10-27T12:10:17.571Z)
Latitude
-0.00004°
Longitude
61.14579°
Altitude
508.379 km
Speed
7.613 km/s
True Right ascension
18h 39m 18s
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
15:51:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
523.291 km
Perigee altitude
492.968 km
Semi-major axis
6,886.267 km
Eccentricity
0.0022
Inclination
97.5517°
RAAN
279.827°
Arg. of periapsis
67.5187°
True anomaly
292.60473°
Mean anomaly
292.8375°
Eccentric anomaly
292.72114°
Mean motion
3.79811 °/min
Orbital period
94.78 mins
BSTAR
0.00077685
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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.ICUBE 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-27 21:49:15.849Z | 102.084° ESE | 2025-10-27 21:51:15.849Z | 66.161° ENE | 15.447° | 2025-10-27 21:53:15.849Z | 31.267° NE |
| 4 mins | 2025-10-27 23:23:15.849Z | 219.094° SW | 2025-10-27 23:25:15.849Z | 274.68° WNW | 25.827° | 2025-10-27 23:27:15.849Z | 317.151° NNW |
| 4 mins | 2025-10-28 10:54:15.849Z | 57.389° ENE | 2025-10-28 10:56:15.849Z | 102.443° ESE | 21.113° | 2025-10-28 10:58:15.849Z | 141.601° SSE |
| 4 mins | 2025-10-28 12:28:15.849Z | 324.178° NNW | 2025-10-28 12:30:15.849Z | 280.346° WNW | 19.406° | 2025-10-28 12:32:15.849Z | 244.879° WSW |
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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