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 35869U 09049E 23081.48635356 .00000214 00000-0 11468-3 0 9997
2 35869 98.5703 47.7300 0005399 123.2839 236.8857 14.22596149701314
| Epoch (UTC): | 22 March 2023 11:40:20 |
| Eccentricity: | 0.0005399 |
| inclination: | 98.5703° |
| perigee height: | 813 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 47.7300° |
| argument of perigee: | 123.2839° |
| revolutions per day: | 14.22596149 |
| mean anomaly at epoch: | 236.8857° |
| orbit number at epoch: | 70131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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