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 35935U 09051E 23340.16711205 .00001149 00000-0 26538-3 0 9997
2 35935 98.4973 215.4376 0007184 208.1517 151.9293 14.57142694754008
| Epoch (UTC): | 06 December 2023 04:00:38 |
| Eccentricity: | 0.0007184 |
| inclination: | 98.4973° |
| perigee height: | 697 km |
| apogee height: | 707 km |
| right ascension of ascending node: | 215.4376° |
| argument of perigee: | 208.1517° |
| revolutions per day: | 14.57142694 |
| mean anomaly at epoch: | 151.9293° |
| orbit number at epoch: | 75400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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