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 22227.76575901 .00000012 00000-0 25287-4 0 9992
2 25634 98.3940 238.8964 0010900 142.2853 217.9090 14.19444355215455
| Epoch (UTC): | 15 August 2022 18:22:41 |
| Eccentricity: | 0.0010900 |
| inclination: | 98.3940° |
| perigee height: | 819 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 238.8964° |
| argument of perigee: | 142.2853° |
| revolutions per day: | 14.19444355 |
| mean anomaly at epoch: | 217.9090° |
| orbit number at epoch: | 21545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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