CE-SAT-IE, 58987
Orbit data source: Space-Track
CE-SAT-IE, 58987 is a payload satellite owned by Canon STL (JP) in SSO that was launched on Sat, 17 Feb 2024 UTC via a H3-22S launch vehicle from the Tanegashima Space Center (TNSTA). 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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58987 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Canon STL
Mission
Operational Commercial Imaging
Bus & Motor
CE-SAT, Unknown motor
Mass
70 kg wet, 70 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.525 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CE-SAT-IE
1 58987U 24032A 26172.39385311 .00000311 00000-0 62095-4 0 9990
2 58987 97.9964 226.9867 0004049 76.4745 283.6911 14.68289076125451Epoch: 2026-06-21T09:27Z
TLE epoch observation values (Epoch: 2026-06-21T09:27:08.908Z)
Latitude
-0.00005°
Longitude
175.60483°
Altitude
668.864 km
Speed
7.523 km/s
True Right ascension
15h 07m 56s
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
21:27:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
666.447 km
Perigee altitude
660.745 km
Semi-major axis
7,041.733 km
Eccentricity
0.0004
Inclination
97.9964°
RAAN
226.9867°
Arg. of periapsis
76.4745°
True anomaly
283.64601°
Mean anomaly
283.6911°
Eccentric anomaly
283.66856°
Mean motion
3.67302 °/min
Orbital period
98.01 mins
BSTAR
0.000062095
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Other satellites on launch #32 in the year 2024 (2024-02-17 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.CE-SAT-IE 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 15:29:21.573Z | 53.966° ENE | 2026-06-22 15:32:21.573Z | 99.003° ESE | 17.376° | 2026-06-22 15:34:21.573Z | 128.697° SE |
| 7 mins | 2026-06-22 17:06:21.573Z | 348.691° N | 2026-06-22 17:09:21.573Z | 282.893° WNW | 32.796° | 2026-06-22 17:13:21.573Z | 219.927° SW |
| 4 mins | 2026-06-23 02:31:21.573Z | 85.201° E | 2026-06-23 02:32:21.573Z | 69.503° E | 16.307° | 2026-06-23 02:35:21.573Z | 26.67° NE |
| 7 mins | 2026-06-23 04:06:21.573Z | 194.756° SSW | 2026-06-23 04:09:21.573Z | 263.798° W | 35.806° | 2026-06-23 04:13:21.573Z | 333.566° NNW |
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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