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 23158.54222532 .00000958 00000-0 22078-3 0 9996
2 35933 98.5153 30.0079 0006836 55.7024 304.4820 14.57622846727968
| Epoch (UTC): | 07 June 2023 13:00:48 |
| Eccentricity: | 0.0006836 |
| inclination: | 98.5153° |
| perigee height: | 696 km |
| apogee height: | 706 km |
| right ascension of ascending node: | 30.0079° |
| argument of perigee: | 55.7024° |
| revolutions per day: | 14.57622846 |
| mean anomaly at epoch: | 304.4820° |
| orbit number at epoch: | 72796 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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