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 25544U 98067A 23337.08337719 .00021458 00000-0 38174-3 0 9992
2 25544 51.6426 211.9904 0001326 5.6465 142.9017 15.50089461427983
| Epoch (UTC): | 03 December 2023 02:00:03 |
| Eccentricity: | 0.0001326 |
| inclination: | 51.6426° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 211.9904° |
| argument of perigee: | 5.6465° |
| revolutions per day: | 15.50089461 |
| mean anomaly at epoch: | 142.9017° |
| orbit number at epoch: | 42798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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