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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Identifier
Orbit
Country
PK / 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: 14 hours ago
TLE from 14 hours ago
0 PAKTES 1A
1 43529U 18056A 26258.57106384 .00001277 00000-0 10919-3 0 9990
2 43529 98.1374 58.9943 0021361 174.6839 185.4614 14.99409388445463Epoch: 2026-09-15T13:42Z
TLE epoch observation values (Epoch: 2026-09-15T13:42:19.915Z)
Latitude
-0°
Longitude
-141.12378°
Altitude
586.536 km
Speed
7.559 km/s
True Right ascension
03h 55m 58s
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
20:01:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.579 km
Perigee altitude
550.913 km
Semi-major axis
6,943.883 km
Eccentricity
0.00214
Inclination
98.1374°
RAAN
58.9943°
Arg. of periapsis
174.6839°
True anomaly
185.43816°
Mean anomaly
185.4614°
Eccentric anomaly
185.44978°
Mean motion
3.75094 °/min
Orbital period
95.98 mins
BSTAR
0.00010919
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Other satellites on launch #56 in the year 2018 (2018-07-09 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.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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-16 10:38:27.428Z | 158.525° S | 2026-09-16 10:42:27.428Z | 77.297° E | 71.052° | 2026-09-16 10:46:27.428Z | 351.922° N |
| 5 mins | 2026-09-16 23:55:27.428Z | 359.446° N | 2026-09-16 23:57:27.428Z | 289.644° WNW | 64.666° | 2026-09-17 00:00:27.428Z | 206.512° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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