PAUSAT-1, 62653
Orbit data source: Space-Track
PAUSAT-1, 62653 is a Turkish payload satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62653 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / TURKRelated business
Manufacturer
ITUTR/PAU
Mission
Operational Amateur Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~30 kg wet, ~30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.124 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 PAUSAT-1
1 62653U 25009AW 25300.90773871 .00006563 00000-0 29829-3 0 9993
2 62653 97.4172 18.9780 0002991 75.4809 284.6759 15.21083186 43442Epoch: 2025-10-27T21:47Z
TLE epoch observation values (Epoch: 2025-10-27T21:47:08.624Z)
Latitude
0.00004°
Longitude
15.68922°
Altitude
505.143 km
Speed
7.612 km/s
True Right ascension
01h 15m 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
01:27:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.594 km
Perigee altitude
497.48 km
Semi-major axis
6,877.674 km
Eccentricity
0.0003
Inclination
97.4172°
RAAN
18.978°
Arg. of periapsis
75.4809°
True anomaly
284.64274°
Mean anomaly
284.6759°
Eccentric anomaly
284.65932°
Mean motion
3.80523 °/min
Orbital period
94.61 mins
BSTAR
0.00029829
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.PAUSAT-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 17:18:34.128Z | 51.412° ENE | 2025-10-28 17:20:34.128Z | 84.86° E | 16.448° | 2025-10-28 17:22:34.128Z | 124.402° SE |
| 4 mins | 2025-10-28 18:53:34.128Z | 321.479° NNW | 2025-10-28 18:54:34.128Z | 295.621° NW | 24.085° | 2025-10-28 18:57:34.128Z | 233.535° WSW |
| 5 mins | 2025-10-29 05:30:34.128Z | 179.705° S | 2025-10-29 05:32:34.128Z | 303.501° NW | 42.478° | 2025-10-29 05:35:34.128Z | 343.48° N |
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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