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 23657U 95046A 22139.13433684 .00001488 00000-0 16427-3 0 9990
2 23657 82.5287 11.9730 0020320 250.2056 109.6970 14.86668602444051
| Epoch (UTC): | 19 May 2022 03:13:26 |
| Eccentricity: | 0.0020320 |
| inclination: | 82.5287° |
| perigee height: | 594 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 11.9730° |
| argument of perigee: | 250.2056° |
| revolutions per day: | 14.86668602 |
| mean anomaly at epoch: | 109.6970° |
| orbit number at epoch: | 44405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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