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 22176.48232896 .00000031 00000-0 00000-0 0 9996
2 35943 0.0653 69.4210 0002728 33.2420 47.5985 1.00269917 46749
| Epoch (UTC): | 25 June 2022 11:34:33 |
| Eccentricity: | 0.0002728 |
| inclination: | 0.0653° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 69.4210° |
| argument of perigee: | 33.2420° |
| revolutions per day: | 1.00269917 |
| mean anomaly at epoch: | 47.5985° |
| orbit number at epoch: | 4674 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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