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 22179.35801735 .00008676 00000-0 16125-3 0 9998
2 25544 51.6436 281.2631 0004568 306.2491 161.7961 15.49741312346919
| Epoch (UTC): | 28 June 2022 08:35:32 |
| Eccentricity: | 0.0004568 |
| inclination: | 51.6436° |
| perigee height: | 414 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 281.2631° |
| argument of perigee: | 306.2491° |
| revolutions per day: | 15.49741312 |
| mean anomaly at epoch: | 161.7961° |
| orbit number at epoch: | 34691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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