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 22140.41947059 .00000206 00000-0 11045-3 0 9999
2 26931 67.0493 130.7573 0007962 267.6566 92.3624 14.30698146 77394
| Epoch (UTC): | 20 May 2022 10:04:02 |
| Eccentricity: | 0.0007962 |
| inclination: | 67.0493° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 130.7573° |
| argument of perigee: | 267.6566° |
| revolutions per day: | 14.30698146 |
| mean anomaly at epoch: | 92.3624° |
| orbit number at epoch: | 7739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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