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 36868U 10039A 23270.27301413 .00000015 00000-0 00000-0 0 9995
2 36868 5.7073 80.6433 0006013 77.9382 309.5010 1.00271835 43692
| Epoch (UTC): | 27 September 2023 06:33:08 |
| Eccentricity: | 0.0006013 |
| inclination: | 5.7073° |
| perigee height: | 35761 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 80.6433° |
| argument of perigee: | 77.9382° |
| revolutions per day: | 1.00271835 |
| mean anomaly at epoch: | 309.5010° |
| orbit number at epoch: | 4369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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