MISRSAT-2, 58497
Orbit data source: Space-Track
MISRSAT-2, 58497 is a payload satellite owned by EgSA (EG) in SSO that was launched on Mon, 04 Dec 2023 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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58497 intel report (Beta)
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Identifier
Orbit
Country
EG / EGYPRelated business
Manufacturer
NCSC/DFHZ
Mission
Operational Civil Imaging
Bus & Motor
CAST-2000?, Unknown motor
Mass
~350 kg wet, ~350 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
2.815 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 MISRSAT-2
1 58497U 23187B 26172.51077683 .00000836 00000-0 10868-3 0 9992
2 58497 97.9271 254.4076 0012181 128.6841 231.5464 14.83251962137682Epoch: 2026-06-21T12:15Z
TLE epoch observation values (Epoch: 2026-06-21T12:15:31.118Z)
Latitude
-0.00002°
Longitude
160.81794°
Altitude
627.411 km
Speed
7.542 km/s
True Right ascension
16h 57m 37s
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
12:45:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.635 km
Perigee altitude
607.596 km
Semi-major axis
6,994.253 km
Eccentricity
0.00122
Inclination
97.9271°
RAAN
254.4076°
Arg. of periapsis
128.6841°
True anomaly
231.43719°
Mean anomaly
231.5464°
Eccentric anomaly
231.49179°
Mean motion
3.71049 °/min
Orbital period
97.02 mins
BSTAR
0.00010868
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Other satellites on launch #187 in the year 2023 (2023-12-04 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.MISRSAT-2 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 | 2026-06-22 04:35:32.967Z | 117.635° SE | 2026-06-22 04:38:32.967Z | 70.481° E | 21.225° | 2026-06-22 04:41:32.967Z | 20.547° NNE |
| 5 mins | 2026-06-22 06:12:32.967Z | 219.27° SW | 2026-06-22 06:14:32.967Z | 262.305° W | 26.228° | 2026-06-22 06:17:32.967Z | 318.314° NNW |
| 6 mins | 2026-06-22 17:59:32.967Z | 35.837° NE | 2026-06-22 18:01:32.967Z | 81.42° E | 35.322° | 2026-06-22 18:05:32.967Z | 171.613° S |
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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