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 22338.51774452 .00000219 00000-0 62997-4 0 9991
2 00029 48.3808 19.9497 0023385 124.8426 235.4690 14.74845043351368
| Epoch (UTC): | 04 December 2022 12:25:33 |
| Eccentricity: | 0.0023385 |
| inclination: | 48.3808° |
| perigee height: | 629 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 19.9497° |
| argument of perigee: | 124.8426° |
| revolutions per day: | 14.74845043 |
| mean anomaly at epoch: | 235.4690° |
| orbit number at epoch: | 35136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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