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 22146.13414207 .00001178 00000-0 12949-3 0 9999
2 23657 82.5279 5.3882 0020644 225.5312 134.4217 14.86687047445095
| Epoch (UTC): | 26 May 2022 03:13:09 |
| Eccentricity: | 0.0020644 |
| inclination: | 82.5279° |
| perigee height: | 594 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 5.3882° |
| argument of perigee: | 225.5312° |
| revolutions per day: | 14.86687047 |
| mean anomaly at epoch: | 134.4217° |
| orbit number at epoch: | 44509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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