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 45578U 26145.58355434 +.00000000 +00000-0 +88530-3 0 00004
2 45578 53.0470 53.5597 0005643 62.9591 297.1997 15.60575246 09
| Epoch (UTC): | 25 May 2026 14:00:19 |
| Eccentricity: | 0.0005643 |
| inclination: | 53.0470° |
| perigee height: | 382 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 53.5597° |
| argument of perigee: | 62.9591° |
| revolutions per day: | 15.60575246 |
| mean anomaly at epoch: | 297.1997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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