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 46986U 99025EZL 22178.36660686 .00000763 00000-0 23250-3 0 9990
2 46986 98.3710 216.9607 0117180 83.0562 278.3940 14.40845677451588
| Epoch (UTC): | 27 June 2022 08:47:54 |
| Eccentricity: | 0.0117180 |
| inclination: | 98.3710° |
| perigee height: | 672 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 216.9607° |
| argument of perigee: | 83.0562° |
| revolutions per day: | 14.40845677 |
| mean anomaly at epoch: | 278.3940° |
| orbit number at epoch: | 45158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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