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 23157.68318566 .00000813 00000-0 19282-3 0 9998
2 35935 98.5253 29.0783 0009180 60.4201 299.7910 14.56671545727466
| Epoch (UTC): | 06 June 2023 16:23:47 |
| Eccentricity: | 0.0009180 |
| inclination: | 98.5253° |
| perigee height: | 697 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 29.0783° |
| argument of perigee: | 60.4201° |
| revolutions per day: | 14.56671545 |
| mean anomaly at epoch: | 299.7910° |
| orbit number at epoch: | 72746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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