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 25989U 99066A 22148.54987739 -.00000209 00000-0 00000-0 0 9994
2 25989 70.1527 305.0514 6067523 87.0339 359.9355 0.50127007 15584
| Epoch (UTC): | 28 May 2022 13:11:49 |
| Eccentricity: | 0.6067523 |
| inclination: | 70.1527° |
| perigee height: | 19946 km |
| apogee height: | 101177 km |
| right ascension of ascending node: | 305.0514° |
| argument of perigee: | 87.0339° |
| revolutions per day: | 0.50127007 |
| mean anomaly at epoch: | 359.9355° |
| orbit number at epoch: | 1558 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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