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 22269.80731582 .00010085 00000-0 18249-3 0 9996
2 25544 51.6432 193.1196 0002434 297.6773 158.1115 15.50305187360946
| Epoch (UTC): | 26 September 2022 19:22:32 |
| Eccentricity: | 0.0002434 |
| inclination: | 51.6432° |
| perigee height: | 414 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 193.1196° |
| argument of perigee: | 297.6773° |
| revolutions per day: | 15.50305187 |
| mean anomaly at epoch: | 158.1115° |
| orbit number at epoch: | 36094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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