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 35933U 09051C 23331.64102781 .00002134 00000-0 47392-3 0 9997
2 35933 98.4880 206.8579 0004563 229.3484 130.7318 14.58096217753101
| Epoch (UTC): | 27 November 2023 15:23:04 |
| Eccentricity: | 0.0004563 |
| inclination: | 98.4880° |
| perigee height: | 696 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 206.8579° |
| argument of perigee: | 229.3484° |
| revolutions per day: | 14.58096217 |
| mean anomaly at epoch: | 130.7318° |
| orbit number at epoch: | 75310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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