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 is defined by the following mean orbital elements,
1 25979U 26074.19009815 +.00000000 +00000-0 +71918-3 0 00006
2 25979 98.1631 156.8566 0004752 75.2054 284.9711 15.31605871 09
| Epoch (UTC): | 15 March 2026 04:33:44 |
| Eccentricity: | 0.0004752 |
| inclination: | 98.1631° |
| perigee height: | 468 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 156.8566° |
| argument of perigee: | 75.2054° |
| revolutions per day: | 15.31605871 |
| mean anomaly at epoch: | 284.9711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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