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 21016.60477425 .00000289 00000-0 27257-4 0 9990
2 29507 97.7171 43.4289 0046107 165.2098 195.0486 15.00619834777333
| Epoch (UTC): | 16 January 2021 14:30:52 |
| Eccentricity: | 0.0046107 |
| inclination: | 97.7171° |
| perigee height: | 533 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 43.4289° |
| argument of perigee: | 165.2098° |
| revolutions per day: | 15.00619834 |
| mean anomaly at epoch: | 195.0486° |
| orbit number at epoch: | 77733 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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