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 22228.93504921 .00005648 00000-0 10612-3 0 9995
2 25544 51.6421 35.6401 0005525 129.3747 328.9951 15.50203667354600
| Epoch (UTC): | 16 August 2022 22:26:28 |
| Eccentricity: | 0.0005525 |
| inclination: | 51.6421° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 35.6401° |
| argument of perigee: | 129.3747° |
| revolutions per day: | 15.50203667 |
| mean anomaly at epoch: | 328.9951° |
| orbit number at epoch: | 35460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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