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 65632U 26145.47948742 +.00000000 +00000-0 +10297-2 0 00009
2 65632 53.1584 310.7028 0001038 73.7446 286.3668 15.30234288 09
| Epoch (UTC): | 25 May 2026 11:30:27 |
| Eccentricity: | 0.0001038 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.7028° |
| argument of perigee: | 73.7446° |
| revolutions per day: | 15.30234288 |
| mean anomaly at epoch: | 286.3668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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