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: 7 hours ago
TLE from 7 hours ago
0 PAKTES 1A
1 43529U 18056A 26078.94925472 .00002096 00000-0 17939-3 0 9997
2 43529 98.1122 231.7262 0021331 48.5224 311.7824 14.98609537418557Epoch: 2026-03-19T22:46Z
TLE epoch observation values (Epoch: 2026-03-19T22:46:55.607Z)
Latitude
-0.00008°
Longitude
72.50318°
Altitude
564.37 km
Speed
7.584 km/s
True Right ascension
15h 26m 54s
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
10:38:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.035 km
Perigee altitude
553.4 km
Semi-major axis
6,946.354 km
Eccentricity
0.00213
Inclination
98.1122°
RAAN
231.7262°
Arg. of periapsis
48.5224°
True anomaly
311.59981°
Mean anomaly
311.7824°
Eccentric anomaly
311.69114°
Mean motion
3.74893 °/min
Orbital period
96.03 mins
BSTAR
0.00017939
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-20 10:07:24.475Z | 166.58° S | 2026-03-20 10:10:24.475Z | 171.796° S | 44.313° | 2026-03-20 10:14:24.475Z | 346.929° N |
| 6 mins | 2026-03-20 23:23:24.475Z | 354.759° N | 2026-03-20 23:26:24.475Z | 265.667° W | 36.278° | 2026-03-20 23:29:24.475Z | 214.042° 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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