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 22181.87396301 -.00000005 00000-0 29714-4 0 9993
2 26931 67.0519 23.7576 0007427 261.7035 98.3224 14.30712294 83322
| Epoch (UTC): | 30 June 2022 20:58:30 |
| Eccentricity: | 0.0007427 |
| inclination: | 67.0519° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 23.7576° |
| argument of perigee: | 261.7035° |
| revolutions per day: | 14.30712294 |
| mean anomaly at epoch: | 98.3224° |
| orbit number at epoch: | 8332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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