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 21691U 91045E 24263.00387774 .00003164 00000-0 77832-3 0 9995
2 21691 89.7835 270.0089 0016310 155.8660 236.3256 14.52056616748461
| Epoch (UTC): | 19 September 2024 00:05:35 |
| Eccentricity: | 0.0016310 |
| inclination: | 89.7835° |
| perigee height: | 707 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 270.0089° |
| argument of perigee: | 155.8660° |
| revolutions per day: | 14.52056616 |
| mean anomaly at epoch: | 236.3256° |
| orbit number at epoch: | 74846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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