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 26932U 01043D 22221.59232764 .00000015 00000-0 37644-4 0 9991
2 26932 67.0558 286.4859 0008569 254.9511 105.0642 14.30431019 89014
| Epoch (UTC): | 09 August 2022 14:12:57 |
| Eccentricity: | 0.0008569 |
| inclination: | 67.0558° |
| perigee height: | 784 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 286.4859° |
| argument of perigee: | 254.9511° |
| revolutions per day: | 14.30431019 |
| mean anomaly at epoch: | 105.0642° |
| orbit number at epoch: | 8901 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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