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 22144.54806250 .00011199 00000-0 20636-3 0 9994
2 25544 51.6431 93.6656 0005128 152.4612 8.3140 15.49653478341516
| Epoch (UTC): | 24 May 2022 13:09:12 |
| Eccentricity: | 0.0005128 |
| inclination: | 51.6431° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 93.6656° |
| argument of perigee: | 152.4612° |
| revolutions per day: | 15.49653478 |
| mean anomaly at epoch: | 8.3140° |
| orbit number at epoch: | 34151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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