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 23081.33270622 .00000013 00000-0 00000+0 0 9996
2 36868 5.2323 83.1240 0003485 347.6115 232.6064 1.00268898 46570
| Epoch (UTC): | 22 March 2023 07:59:05 |
| Eccentricity: | 0.0003485 |
| inclination: | 5.2323° |
| perigee height: | 35772 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 83.1240° |
| argument of perigee: | 347.6115° |
| revolutions per day: | 1.00268898 |
| mean anomaly at epoch: | 232.6064° |
| orbit number at epoch: | 4657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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