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 22140.49861191 .00000104 00000-0 68943-4 0 9993
2 25634 98.3951 156.1564 0011001 46.1600 314.0485 14.19432710203074
| Epoch (UTC): | 20 May 2022 11:58:00 |
| Eccentricity: | 0.0011001 |
| inclination: | 98.3951° |
| perigee height: | 819 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 156.1564° |
| argument of perigee: | 46.1600° |
| revolutions per day: | 14.19432710 |
| mean anomaly at epoch: | 314.0485° |
| orbit number at epoch: | 20307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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