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 21015.53787670 .00000287 00000-0 27142-4 0 9998
2 29507 97.7170 42.3700 0045976 168.9094 191.3154 15.00619079777171
| Epoch (UTC): | 15 January 2021 12:54:32 |
| Eccentricity: | 0.0045976 |
| inclination: | 97.7170° |
| perigee height: | 533 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 42.3700° |
| argument of perigee: | 168.9094° |
| revolutions per day: | 15.00619079 |
| mean anomaly at epoch: | 191.3154° |
| orbit number at epoch: | 77717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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