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 15752U 85041B 23152.89180312 .00000168 00000-0 16522-3 0 9997
2 15752 82.9478 141.6061 0023566 195.9362 164.1054 13.73190260904192
| Epoch (UTC): | 01 June 2023 21:24:11 |
| Eccentricity: | 0.0023566 |
| inclination: | 82.9478° |
| perigee height: | 971 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 141.6061° |
| argument of perigee: | 195.9362° |
| revolutions per day: | 13.73190260 |
| mean anomaly at epoch: | 164.1054° |
| orbit number at epoch: | 90419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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