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 29194U 76103G 22181.46240556 .00000208 00000-0 21376-3 0 9990
2 29194 64.6850 184.8650 0058632 215.1656 144.5533 13.96830780968999
| Epoch (UTC): | 30 June 2022 11:05:51 |
| Eccentricity: | 0.0058632 |
| inclination: | 64.6850° |
| perigee height: | 862 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 184.8650° |
| argument of perigee: | 215.1656° |
| revolutions per day: | 13.96830780 |
| mean anomaly at epoch: | 144.5533° |
| orbit number at epoch: | 96899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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