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 23087.21586238 .00001715 00000-0 38862-3 0 9997
2 35933 98.5265 317.0201 0004508 269.8323 90.2358 14.57438142717577
| Epoch (UTC): | 28 March 2023 05:10:50 |
| Eccentricity: | 0.0004508 |
| inclination: | 98.5265° |
| perigee height: | 698 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 317.0201° |
| argument of perigee: | 269.8323° |
| revolutions per day: | 14.57438142 |
| mean anomaly at epoch: | 90.2358° |
| orbit number at epoch: | 71757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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