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 62557U 26145.06186742 +.00000000 +00000-0 +11344-2 0 00005
2 62557 43.0028 39.5605 0002106 271.7718 88.2908 15.70875142 09
| Epoch (UTC): | 25 May 2026 01:29:05 |
| Eccentricity: | 0.0002106 |
| inclination: | 43.0028° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 39.5605° |
| argument of perigee: | 271.7718° |
| revolutions per day: | 15.70875142 |
| mean anomaly at epoch: | 88.2908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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