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 23342.14016425 .00000940 00000-0 21456-3 0 9999
2 35933 98.4875 217.5735 0005104 192.2018 167.9057 14.58135370754715
| Epoch (UTC): | 08 December 2023 03:21:50 |
| Eccentricity: | 0.0005104 |
| inclination: | 98.4875° |
| perigee height: | 695 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 217.5735° |
| argument of perigee: | 192.2018° |
| revolutions per day: | 14.58135370 |
| mean anomaly at epoch: | 167.9057° |
| orbit number at epoch: | 75471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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