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 25544U 98067A 22185.99100762 .00006188 00000-0 11699-3 0 9994
2 25544 51.6428 248.4132 0004457 332.8385 86.6328 15.49830063347943
| Epoch (UTC): | 04 July 2022 23:47:03 |
| Eccentricity: | 0.0004457 |
| inclination: | 51.6428° |
| perigee height: | 414 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 248.4132° |
| argument of perigee: | 332.8385° |
| revolutions per day: | 15.49830063 |
| mean anomaly at epoch: | 86.6328° |
| orbit number at epoch: | 34794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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