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 26863U 01029A 23091.01994083 -.00000157 00000-0 00000-0 0 9990
2 26863 14.1660 15.1557 0012522 126.8470 56.7727 0.99295258 32209
| Epoch (UTC): | 01 April 2023 00:28:42 |
| Eccentricity: | 0.0012522 |
| inclination: | 14.1660° |
| perigee height: | 36009 km |
| apogee height: | 36115 km |
| right ascension of ascending node: | 15.1557° |
| argument of perigee: | 126.8470° |
| revolutions per day: | 0.99295258 |
| mean anomaly at epoch: | 56.7727° |
| orbit number at epoch: | 3220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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