ISTSAT-1, 60238
Orbit data source: Space-Track
ISTSAT-1, 60238 is a Portuguese payload satellite in LEO that was launched on Tue, 09 Jul 2024 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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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60238 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PT / PORRelated business
Manufacturer
ISTL
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ISTSAT-1
1 60238U 24128D 25309.27251602 .00008078 00000-0 52281-3 0 9994
2 60238 61.9892 275.7120 0055238 87.5760 273.1655 15.07654641 72654Epoch: 2025-11-05T06:32Z
TLE epoch observation values (Epoch: 2025-11-05T06:32:25.384Z)
Latitude
-0.00008°
Longitude
132.85863°
Altitude
543.243 km
Speed
7.592 km/s
True Right ascension
18h 22m 50s
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
20:59:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.524 km
Perigee altitude
504.07 km
Semi-major axis
6,920.434 km
Eccentricity
0.00552
Inclination
61.9892°
RAAN
275.712°
Arg. of periapsis
87.576°
True anomaly
272.53326°
Mean anomaly
273.1655°
Eccentric anomaly
272.8494°
Mean motion
3.77002 °/min
Orbital period
95.49 mins
BSTAR
0.00052281
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Other satellites on launch #128 in the year 2024 (2024-07-09 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.ISTSAT-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 | 2025-11-06 06:55:18.789Z | 7.594° NNE | 2025-11-06 06:57:18.789Z | 41.681° NE | 15.04° | 2025-11-06 06:59:18.789Z | 74.562° E |
| 6 mins | 2025-11-06 08:33:18.789Z | 312.788° NW | 2025-11-06 08:36:18.789Z | 217.311° SW | 39.998° | 2025-11-06 08:39:18.789Z | 159.807° S |
| 6 mins | 2025-11-07 00:06:18.789Z | 246.03° WSW | 2025-11-07 00:08:18.789Z | 289.767° WNW | 33.155° | 2025-11-07 00:12:18.789Z | 22.701° NE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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