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: 7 hours ago
TLE from 7 hours ago
0 ISTSAT-1
1 60238U 24128D 26124.78286708 .00007086 00000-0 42501-3 0 9993
2 60238 61.9894 359.5364 0043797 122.9265 237.6054 15.11046046 99902Epoch: 2026-05-04T18:47Z
TLE epoch observation values (Epoch: 2026-05-04T18:47:19.715Z)
Latitude
-0.00007°
Longitude
-144.9629°
Altitude
551.098 km
Speed
7.578 km/s
True Right ascension
23h 58m 08s
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
09:45:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.199 km
Perigee altitude
501.671 km
Semi-major axis
6,910.072 km
Eccentricity
0.00438
Inclination
61.9894°
RAAN
359.5364°
Arg. of periapsis
122.9265°
True anomaly
237.18287°
Mean anomaly
237.6054°
Eccentric anomaly
237.39401°
Mean motion
3.7785 °/min
Orbital period
95.28 mins
BSTAR
0.00042501
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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 | 2026-05-05 03:18:57.377Z | 274.733° WNW | 2026-05-05 03:20:57.377Z | 236.874° WSW | 16.493° | 2026-05-05 03:22:57.377Z | 204.19° SW |
| 5 mins | 2026-05-05 17:10:57.377Z | 186.283° SSW | 2026-05-05 17:12:57.377Z | 128.154° SE | 37.157° | 2026-05-05 17:15:57.377Z | 50.731° ENE |
| 4 mins | 2026-05-05 18:49:57.377Z | 288.388° WNW | 2026-05-05 18:51:57.377Z | 325.67° NNW | 16.922° | 2026-05-05 18:53:57.377Z | 358.822° N |
| 5 mins | 2026-05-06 01:29:57.377Z | 345.623° N | 2026-05-06 01:31:57.377Z | 38.903° NE | 35.153° | 2026-05-06 01:34:57.377Z | 119.425° SE |
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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