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 25544U 26105.55408208 +.00000000 +00000-0 +10354-3 0 00005
2 25544 51.6327 250.0746 0006583 315.7730 44.2732 15.48924547 09
| Epoch (UTC): | 15 April 2026 13:17:52 |
| Eccentricity: | 0.0006583 |
| inclination: | 51.6327° |
| perigee height: | 415 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 250.0746° |
| argument of perigee: | 315.7730° |
| revolutions per day: | 15.48924547 |
| mean anomaly at epoch: | 44.2732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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