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 23154.49481764 .00000149 00000-0 14484-3 0 9994
2 15752 82.9479 140.4234 0023678 191.4072 168.6549 13.73190680904414
| Epoch (UTC): | 03 June 2023 11:52:32 |
| Eccentricity: | 0.0023678 |
| inclination: | 82.9479° |
| perigee height: | 970 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 140.4234° |
| argument of perigee: | 191.4072° |
| revolutions per day: | 13.73190680 |
| mean anomaly at epoch: | 168.6549° |
| orbit number at epoch: | 90441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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