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 15495U 85009B 23341.50046396 .00000583 00000-0 65807-4 0 9998
2 15495 82.5224 132.0663 0021239 87.8678 272.4969 14.84657892 79448
| Epoch (UTC): | 07 December 2023 12:00:40 |
| Eccentricity: | 0.0021239 |
| inclination: | 82.5224° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 132.0663° |
| argument of perigee: | 87.8678° |
| revolutions per day: | 14.84657892 |
| mean anomaly at epoch: | 272.4969° |
| orbit number at epoch: | 7944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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