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 39087U 13009B 23274.47219260 .00001304 00000-0 45385-3 0 9995
2 39087 98.3781 106.8099 0011279 303.9652 56.0462 14.37000967555191
| Epoch (UTC): | 01 October 2023 11:19:57 |
| Eccentricity: | 0.0011279 |
| inclination: | 98.3781° |
| perigee height: | 760 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 106.8099° |
| argument of perigee: | 303.9652° |
| revolutions per day: | 14.37000967 |
| mean anomaly at epoch: | 56.0462° |
| orbit number at epoch: | 55519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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