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 30277U 99025YN 24257.11264576 .00010218 00000-0 53815-2 0 9992
2 30277 99.0126 320.4263 0128339 23.5178 5.9965 14.10007899903757
| Epoch (UTC): | 13 September 2024 02:42:12 |
| Eccentricity: | 0.0128339 |
| inclination: | 99.0126° |
| perigee height: | 766 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 320.4263° |
| argument of perigee: | 23.5178° |
| revolutions per day: | 14.10007899 |
| mean anomaly at epoch: | 5.9965° |
| orbit number at epoch: | 90375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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