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 24256.77763577 .00001772 00000-0 63327-3 0 9993
2 22676 74.0439 23.7453 0017743 125.0167 235.2654 14.34741197634146
| Epoch (UTC): | 12 September 2024 18:39:47 |
| Eccentricity: | 0.0017743 |
| inclination: | 74.0439° |
| perigee height: | 763 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 23.7453° |
| argument of perigee: | 125.0167° |
| revolutions per day: | 14.34741197 |
| mean anomaly at epoch: | 235.2654° |
| orbit number at epoch: | 63414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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