View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 12508U 81053B 23156.88942773 .00000056 00000-0 41767-4 0 9998
2 12508 82.9573 328.3782 0036369 228.6408 131.1619 13.76443703115076
Epoch (UTC): | 05 June 2023 21:20:46 |
Eccentricity: | 0.0036369 |
inclination: | 82.9573° |
perigee height: | 950 km |
apogee height: | 1003 km |
right ascension of ascending node: | 328.3782° |
argument of perigee: | 228.6408° |
revolutions per day: | 13.76443703 |
mean anomaly at epoch: | 131.1619° |
orbit number at epoch: | 11507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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