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 65753U 26145.55747830 +.00000000 +00000-0 +85029-3 0 00003
2 65753 53.1590 335.7569 0001701 80.7275 279.3918 15.30224405 02
| Epoch (UTC): | 25 May 2026 13:22:46 |
| Eccentricity: | 0.0001701 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.7569° |
| argument of perigee: | 80.7275° |
| revolutions per day: | 15.30224405 |
| mean anomaly at epoch: | 279.3918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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