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 is defined by the following mean orbital elements,
1 29668U 06061A 21187.54762907 .99999999 88006-5 39685-3 0 9996
2 29668 61.1736 172.0554 0243685 261.4665 207.9004 16.18069742109757
| Epoch (UTC): | 06 July 2021 13:08:35 |
| Eccentricity: | 0.0243685 |
| inclination: | 61.1736° |
| perigee height: | 64 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 172.0554° |
| argument of perigee: | 261.4665° |
| revolutions per day: | 16.18069742 |
| mean anomaly at epoch: | 207.9004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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