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 36605U 10030A 23029.69932899 .00001770 00000-0 87444-4 0 9991
2 36605 97.4478 39.0564 0002034 101.1928 317.8869 15.19157460699217
| Epoch (UTC): | 29 January 2023 16:47:02 |
| Eccentricity: | 0.0002034 |
| inclination: | 97.4478° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 39.0564° |
| argument of perigee: | 101.1928° |
| revolutions per day: | 15.19157460 |
| mean anomaly at epoch: | 317.8869° |
| orbit number at epoch: | 69921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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