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 25634U 99008A 22147.54767543 .00000069 00000-0 52029-4 0 9990
2 25634 98.3945 162.8408 0010684 27.1082 333.0651 14.19434291204070
| Epoch (UTC): | 27 May 2022 13:08:39 |
| Eccentricity: | 0.0010684 |
| inclination: | 98.3945° |
| perigee height: | 819 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 162.8408° |
| argument of perigee: | 27.1082° |
| revolutions per day: | 14.19434291 |
| mean anomaly at epoch: | 333.0651° |
| orbit number at epoch: | 20407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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