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 29507U 06046C 21060.01327083 .00000750 00000-0 62736-4 0 9992
2 29507 97.7198 86.5211 0049173 21.7251 338.6044 15.00672162783894
| Epoch (UTC): | 01 March 2021 00:19:06 |
| Eccentricity: | 0.0049173 |
| inclination: | 97.7198° |
| perigee height: | 530 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 86.5211° |
| argument of perigee: | 21.7251° |
| revolutions per day: | 15.00672162 |
| mean anomaly at epoch: | 338.6044° |
| orbit number at epoch: | 78389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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