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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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: 8 hours ago
TLE from 8 hours ago
0 KAZEOSAT 2
1 40010U 14033A 26251.28296660 -.00000151 00000-0 -11724-4 0 9999
2 40010 97.5375 86.4997 0009932 50.3778 309.8314 14.85549803661298Epoch: 2026-09-08T06:47Z
TLE epoch observation values (Epoch: 2026-09-08T06:47:28.314Z)
Latitude
0.00008°
Longitude
-2.71989°
Altitude
610.457 km
Speed
7.556 km/s
True Right ascension
05h 45m 59s
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
06:27:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.818 km
Perigee altitude
601.939 km
Semi-major axis
6,987.015 km
Eccentricity
0.00099
Inclination
97.5375°
RAAN
86.4997°
Arg. of periapsis
50.3778°
True anomaly
309.74393°
Mean anomaly
309.8314°
Eccentric anomaly
309.78767°
Mean motion
3.71626 °/min
Orbital period
96.87 mins
BSTAR
-0.000011724
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-09 01:09:45.730Z | 48.56° ENE | 2026-09-09 01:12:45.730Z | 103.786° ESE | 23.888° | 2026-09-09 01:15:45.730Z | 148.977° SSE |
| 6 mins | 2026-09-09 02:45:45.730Z | 338.071° N | 2026-09-09 02:48:45.730Z | 278.486° WNW | 26.64° | 2026-09-09 02:51:45.730Z | 233.459° WSW |
| 4 mins | 2026-09-09 12:03:45.730Z | 90.52° ESE | 2026-09-09 12:04:45.730Z | 74.332° E | 16.615° | 2026-09-09 12:07:45.730Z | 28.182° NE |
| 6 mins | 2026-09-09 13:38:45.730Z | 206.647° SW | 2026-09-09 13:40:45.730Z | 257.774° W | 40.268° | 2026-09-09 13:44:45.730Z | 332.038° 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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