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 21107.55330652 .00001103 00000-0 89946-4 0 9994
2 29507 97.7278 133.7609 0046582 220.4236 139.3524 15.00772239790973
| Epoch (UTC): | 17 April 2021 13:16:45 |
| Eccentricity: | 0.0046582 |
| inclination: | 97.7278° |
| perigee height: | 532 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 133.7609° |
| argument of perigee: | 220.4236° |
| revolutions per day: | 15.00772239 |
| mean anomaly at epoch: | 139.3524° |
| orbit number at epoch: | 79097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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