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 26931U 01043C 20337.51783278 -.00000002 00000-0 31166-4 0 9999
2 26931 67.0525 68.6793 0007159 274.4698 85.5585 14.30597166 1086
| Epoch (UTC): | 02 December 2020 12:25:40 |
| Eccentricity: | 0.0007159 |
| inclination: | 67.0525° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 68.6793° |
| argument of perigee: | 274.4698° |
| revolutions per day: | 14.30597166 |
| mean anomaly at epoch: | 85.5585° |
| orbit number at epoch: | 108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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