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 27534U 02046A 23083.61514377 .00000076 00000-0 66208-4 0 9992
2 27534 82.9326 123.1021 0036582 16.0671 95.6995 13.72784035 26571
| Epoch (UTC): | 24 March 2023 14:45:48 |
| Eccentricity: | 0.0036582 |
| inclination: | 82.9326° |
| perigee height: | 962 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 123.1021° |
| argument of perigee: | 16.0671° |
| revolutions per day: | 13.72784035 |
| mean anomaly at epoch: | 95.6995° |
| orbit number at epoch: | 2657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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