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 27056U 01058B 23083.80672468 .00000048 00000-0 21506-3 0 9990
2 27056 82.5317 254.7027 0006282 23.7835 336.3546 12.60524720977227
| Epoch (UTC): | 24 March 2023 19:21:41 |
| Eccentricity: | 0.0006282 |
| inclination: | 82.5317° |
| perigee height: | 1416 km |
| apogee height: | 1425 km |
| right ascension of ascending node: | 254.7027° |
| argument of perigee: | 23.7835° |
| revolutions per day: | 12.60524720 |
| mean anomaly at epoch: | 336.3546° |
| orbit number at epoch: | 97722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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