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 00029U 60002B 23084.75233782 .00002222 00000-0 35455-3 0 9996
2 00029 48.3780 214.4913 0024444 241.3401 118.5053 14.75149376367781
| Epoch (UTC): | 25 March 2023 18:03:21 |
| Eccentricity: | 0.0024444 |
| inclination: | 48.3780° |
| perigee height: | 627 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 214.4913° |
| argument of perigee: | 241.3401° |
| revolutions per day: | 14.75149376 |
| mean anomaly at epoch: | 118.5053° |
| orbit number at epoch: | 36778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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