KAZEOSAT 2, 40010
Orbit data source: Space-Track
KAZEOSAT 2, 40010 is a payload satellite owned by Kazkosmos (KZ) in SSO that was launched on Thu, 19 Jun 2014 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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40010 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
KZ / KAZRelated business
Manufacturer
SSTL (Astrium)
Mission
Operational Civil Imaging
Bus & Motor
SSTL-150, AOCS
Mass
177 kg wet, 177 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.5 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 KAZEOSAT 2
1 40010U 14033A 25260.31283528 .00000599 00000-0 76170-4 0 9991
2 40010 97.5630 109.0492 0009712 133.1181 227.0849 14.84955467608457Epoch: 2025-09-17T07:30Z
TLE epoch observation values (Epoch: 2025-09-17T07:30:28.968Z)
Latitude
0.00004°
Longitude
-0.06209°
Altitude
621.392 km
Speed
7.546 km/s
True Right ascension
07h 16m 11s
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
07:01:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.533 km
Perigee altitude
603.957 km
Semi-major axis
6,988.882 km
Eccentricity
0.00097
Inclination
97.563°
RAAN
109.0492°
Arg. of periapsis
133.1181°
True anomaly
227.00346°
Mean anomaly
227.0849°
Eccentric anomaly
227.04417°
Mean motion
3.71477 °/min
Orbital period
96.91 mins
BSTAR
0.00007617
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.KAZEOSAT 2 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 | 2025-09-18 01:53:11.635Z | 51.571° ENE | 2025-09-18 01:56:11.635Z | 99.552° ESE | 17.53° | 2025-09-18 01:58:11.635Z | 131.144° SE |
| 6 mins | 2025-09-18 03:29:11.635Z | 345.611° N | 2025-09-18 03:32:11.635Z | 280.988° WNW | 29.293° | 2025-09-18 03:35:11.635Z | 227.451° 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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