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 35943U 09054B 22026.86050056 .00000032 00000-0 00000-0 0 9999
2 35943 0.0224 97.1808 0001843 222.8773 178.8683 1.00276820 45246
| Epoch (UTC): | 26 January 2022 20:39:07 |
| Eccentricity: | 0.0001843 |
| inclination: | 0.0224° |
| perigee height: | 35777 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 97.1808° |
| argument of perigee: | 222.8773° |
| revolutions per day: | 1.00276820 |
| mean anomaly at epoch: | 178.8683° |
| orbit number at epoch: | 4524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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