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 22676U 93036B 23337.60561939 .00000367 00000-0 13943-3 0 9990
2 22676 74.0405 184.0240 0018764 350.1810 9.8972 14.34442586593393
| Epoch (UTC): | 03 December 2023 14:32:05 |
| Eccentricity: | 0.0018764 |
| inclination: | 74.0405° |
| perigee height: | 763 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 184.0240° |
| argument of perigee: | 350.1810° |
| revolutions per day: | 14.34442586 |
| mean anomaly at epoch: | 9.8972° |
| orbit number at epoch: | 59339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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