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 15944U 85069A 23149.73028891 .00006821 00000-0 24892-3 0 9993
2 15944 82.5050 230.1853 0015907 108.7684 251.5283 15.27833653 67870
| Epoch (UTC): | 29 May 2023 17:31:36 |
| Eccentricity: | 0.0015907 |
| inclination: | 82.5050° |
| perigee height: | 471 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 230.1853° |
| argument of perigee: | 108.7684° |
| revolutions per day: | 15.27833653 |
| mean anomaly at epoch: | 251.5283° |
| orbit number at epoch: | 6787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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