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 36089U 09061B 23331.86506446 .00001257 00000-0 31876-3 0 9996
2 36089 98.3323 294.3382 0080702 16.0730 344.2997 14.50645589742829
| Epoch (UTC): | 27 November 2023 20:45:41 |
| Eccentricity: | 0.0080702 |
| inclination: | 98.3323° |
| perigee height: | 666 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 294.3382° |
| argument of perigee: | 16.0730° |
| revolutions per day: | 14.50645589 |
| mean anomaly at epoch: | 344.2997° |
| orbit number at epoch: | 74282 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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