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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ISTSAT-1
1 60238U 24128D 26264.86283589 .00003921 00000-0 23471-3 0 9990
2 60238 61.9868 224.0240 0024189 148.9006 211.3528 15.12609719121080Epoch: 2026-09-21T20:42Z
TLE epoch observation values (Epoch: 2026-09-21T20:42:29.020Z)
Latitude
0°
Longitude
-87.33348°
Altitude
544.301 km
Speed
7.583 km/s
True Right ascension
14h 56m 05s
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
00:05:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.874 km
Perigee altitude
510.468 km
Semi-major axis
6,905.308 km
Eccentricity
0.00242
Inclination
61.9868°
RAAN
224.024°
Arg. of periapsis
148.9006°
True anomaly
211.20895°
Mean anomaly
211.3528°
Eccentric anomaly
211.28084°
Mean motion
3.78241 °/min
Orbital period
95.18 mins
BSTAR
0.00023471
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-22 08:21:25.715Z | 310.975° NW | 2026-09-22 08:24:25.715Z | 257.461° W | 45.089° | 2026-09-22 08:28:25.715Z | 165.198° S |
| 4 mins | 2026-09-22 22:14:25.715Z | 148.665° SSE | 2026-09-22 22:16:25.715Z | 111.564° ESE | 19.205° | 2026-09-22 22:18:25.715Z | 77.059° E |
| 6 mins | 2026-09-22 23:51:25.715Z | 248.187° W | 2026-09-22 23:54:25.715Z | 320.77° NNW | 38.304° | 2026-09-22 23:57:25.715Z | 18.383° NNE |
| 4 mins | 2026-09-23 06:33:25.715Z | 20.144° NNE | 2026-09-23 06:34:25.715Z | 41.201° NE | 20.323° | 2026-09-23 06:37:25.715Z | 91.927° ESE |
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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