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 25979U 99064C 24255.55166427 .00020338 00000-0 11991-2 0 9993
2 25979 98.2408 278.1171 0008000 141.9565 218.2229 15.11586623345962
| Epoch (UTC): | 11 September 2024 13:14:23 |
| Eccentricity: | 0.0008000 |
| inclination: | 98.2408° |
| perigee height: | 526 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 278.1171° |
| argument of perigee: | 141.9565° |
| revolutions per day: | 15.11586623 |
| mean anomaly at epoch: | 218.2229° |
| orbit number at epoch: | 34596 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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