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 21666U 91059A 23083.54957400 .00000091 00000-0 81400-4 0 9992
2 21666 82.9023 266.1072 0023830 253.9405 159.9748 13.73380440582770
| Epoch (UTC): | 24 March 2023 13:11:23 |
| Eccentricity: | 0.0023830 |
| inclination: | 82.9023° |
| perigee height: | 970 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 266.1072° |
| argument of perigee: | 253.9405° |
| revolutions per day: | 13.73380440 |
| mean anomaly at epoch: | 159.9748° |
| orbit number at epoch: | 58277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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