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 21108.55341849 .00001178 00000-0 95715-4 0 9998
2 29507 97.7280 134.7554 0046617 216.9674 142.8335 15.00775147791129
| Epoch (UTC): | 18 April 2021 13:16:55 |
| Eccentricity: | 0.0046617 |
| inclination: | 97.7280° |
| perigee height: | 532 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 134.7554° |
| argument of perigee: | 216.9674° |
| revolutions per day: | 15.00775147 |
| mean anomaly at epoch: | 142.8335° |
| orbit number at epoch: | 79112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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