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 21025.80673684 .00000462 00000-0 40591-4 0 9996
2 29507 97.7173 52.5622 0047277 133.7812 226.7338 15.00627465778710
| Epoch (UTC): | 25 January 2021 19:21:42 |
| Eccentricity: | 0.0047277 |
| inclination: | 97.7173° |
| perigee height: | 532 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 52.5622° |
| argument of perigee: | 133.7812° |
| revolutions per day: | 15.00627465 |
| mean anomaly at epoch: | 226.7338° |
| orbit number at epoch: | 77871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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