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 22180.70987817 .00008790 00000-0 16312-3 0 9990
2 25544 51.6438 274.5677 0004456 312.0413 143.1698 15.49766325347127
| Epoch (UTC): | 29 June 2022 17:02:13 |
| Eccentricity: | 0.0004456 |
| inclination: | 51.6438° |
| perigee height: | 414 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 274.5677° |
| argument of perigee: | 312.0413° |
| revolutions per day: | 15.49766325 |
| mean anomaly at epoch: | 143.1698° |
| orbit number at epoch: | 34712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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