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 10521U 77119B 23159.47027201 .00000269 00000-0 91442-4 0 9998
2 10521 74.0255 187.3505 0020379 24.6037 335.6086 14.41178300386249
| Epoch (UTC): | 08 June 2023 11:17:11 |
| Eccentricity: | 0.0020379 |
| inclination: | 74.0255° |
| perigee height: | 740 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 187.3505° |
| argument of perigee: | 24.6037° |
| revolutions per day: | 14.41178300 |
| mean anomaly at epoch: | 335.6086° |
| orbit number at epoch: | 38624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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