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 23029.42599014 .00000026 00000-0 00000+0 0 9999
2 35943 0.0723 79.7580 0002541 228.7573 36.2153 1.00273099 48889
| Epoch (UTC): | 29 January 2023 10:13:25 |
| Eccentricity: | 0.0002541 |
| inclination: | 0.0723° |
| perigee height: | 35775 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 79.7580° |
| argument of perigee: | 228.7573° |
| revolutions per day: | 1.00273099 |
| mean anomaly at epoch: | 36.2153° |
| orbit number at epoch: | 4888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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