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 00899U 64064A 23083.21028138 .00000851 00000-0 73930-3 0 9996
2 00899 79.6935 338.6590 0121147 0.9833 359.1532 13.82363533941751
| Epoch (UTC): | 24 March 2023 05:02:48 |
| Eccentricity: | 0.0121147 |
| inclination: | 79.6935° |
| perigee height: | 866 km |
| apogee height: | 1044 km |
| right ascension of ascending node: | 338.6590° |
| argument of perigee: | 0.9833° |
| revolutions per day: | 13.82363533 |
| mean anomaly at epoch: | 359.1532° |
| orbit number at epoch: | 94175 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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