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 29U 60002B 22027.78238688 .00000039 00000-0 36650-4 0 9998
2 29 48.3803 47.1194 0024527 234.9384 124.9227 14.74512144305624
| Epoch (UTC): | 27 January 2022 18:46:38 |
| Eccentricity: | 0.0024527 |
| inclination: | 48.3803° |
| perigee height: | 629 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 47.1194° |
| argument of perigee: | 234.9384° |
| revolutions per day: | 14.74512144 |
| mean anomaly at epoch: | 124.9227° |
| orbit number at epoch: | 30562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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