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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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: 8 hours ago
TLE from 8 hours ago
0 ISTSAT-1
1 60238U 24128D 26084.93859644 .00005405 00000-0 33132-3 0 9993
2 60238 61.9874 140.2384 0047451 114.7413 245.8631 15.10487901 93883Epoch: 2026-03-25T22:31Z
TLE epoch observation values (Epoch: 2026-03-25T22:31:34.732Z)
Latitude
-0.00002°
Longitude
-21.05104°
Altitude
550.031 km
Speed
7.58 km/s
True Right ascension
09h 20m 57s
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
11:45:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.435 km
Perigee altitude
500.841 km
Semi-major axis
6,911.775 km
Eccentricity
0.00475
Inclination
61.9874°
RAAN
140.2384°
Arg. of periapsis
114.7413°
True anomaly
245.3681°
Mean anomaly
245.8631°
Eccentric anomaly
245.61548°
Mean motion
3.7771 °/min
Orbital period
95.31 mins
BSTAR
0.00033132
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-26 06:39:28.074Z | 260.915° W | 2026-03-26 06:42:28.074Z | 318.704° NNW | 23.496° | 2026-03-26 06:45:28.074Z | 11.733° NNE |
| 4 mins | 2026-03-26 13:21:28.074Z | 4.932° NNE | 2026-03-26 13:23:28.074Z | 57.725° ENE | 25.282° | 2026-03-26 13:25:28.074Z | 98.711° ESE |
| 4 mins | 2026-03-26 14:59:28.074Z | 282.546° WNW | 2026-03-26 15:01:28.074Z | 238.533° WSW | 22.002° | 2026-03-26 15:03:28.074Z | 198.296° SSW |
| 5 mins | 2026-03-27 04:52:28.074Z | 165.977° S | 2026-03-27 04:54:28.074Z | 106.367° ESE | 29.597° | 2026-03-27 04:57:28.074Z | 54.428° ENE |
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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