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 23271.21033594 .00000311 00000-0 11974-3 0 9996
2 22676 74.0412 305.5544 0017668 133.4885 226.7739 14.34377232584187
| Epoch (UTC): | 28 September 2023 05:02:53 |
| Eccentricity: | 0.0017668 |
| inclination: | 74.0412° |
| perigee height: | 764 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 305.5544° |
| argument of perigee: | 133.4885° |
| revolutions per day: | 14.34377232 |
| mean anomaly at epoch: | 226.7739° |
| orbit number at epoch: | 58418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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