PAKTES 1A, 43529
Orbit data source: Space-Track
PAKTES 1A, 43529 is a payload satellite owned by SUPARCO (PK) in SSO that was launched on Mon, 09 Jul 2018 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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43529 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / PAKIRelated business
Manufacturer
SUPARCO
Mission
Operational Civil Imaging
Bus & Motor
PAKTES, Unknown motor
Mass
285 kg wet, 285 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.0 m
Radar Cross Section
5.935 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 PAKTES 1A
1 43529U 18056A 25341.96871687 .00003186 00000-0 27414-3 0 9999
2 43529 98.1033 125.7953 0022607 29.9830 330.2680 14.97970794403285Epoch: 2025-12-07T23:14Z
TLE epoch observation values (Epoch: 2025-12-07T23:14:57.137Z)
Latitude
-0.00007°
Longitude
60.08275°
Altitude
562.566 km
Speed
7.587 km/s
True Right ascension
08h 23m 10s
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
08:44:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.901 km
Perigee altitude
554.485 km
Semi-major axis
6,948.33 km
Eccentricity
0.00226
Inclination
98.1033°
RAAN
125.7953°
Arg. of periapsis
29.983°
True anomaly
330.13921°
Mean anomaly
330.268°
Eccentric anomaly
330.20363°
Mean motion
3.74733 °/min
Orbital period
96.07 mins
BSTAR
0.00027414
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Other satellites on launch #56 in the year 2018 (2018-07-09 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.PAKTES 1A 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 | 2025-12-08 10:35:35.479Z | 213.798° SW | 2025-12-08 10:38:35.479Z | 265.003° W | 20.495° | 2025-12-08 10:41:35.479Z | 315.56° NNW |
| 6 mins | 2025-12-08 22:16:35.479Z | 35.738° NE | 2025-12-08 22:18:35.479Z | 80.31° E | 34.396° | 2025-12-08 22:22:35.479Z | 171.609° S |
| 5 mins | 2025-12-09 09:04:35.479Z | 108.476° ESE | 2025-12-09 09:06:35.479Z | 60.571° ENE | 24.386° | 2025-12-09 09:09:35.479Z | 11.616° NNE |
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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