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 22626U 93024A 23151.51442768 .00001656 00000-0 16928-3 0 9992
2 22626 82.5195 150.3740 0020272 97.6616 262.6905 14.89828329629201
| Epoch (UTC): | 31 May 2023 12:20:46 |
| Eccentricity: | 0.0020272 |
| inclination: | 82.5195° |
| perigee height: | 584 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 150.3740° |
| argument of perigee: | 97.6616° |
| revolutions per day: | 14.89828329 |
| mean anomaly at epoch: | 262.6905° |
| orbit number at epoch: | 62920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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