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 59691U 26145.56029899 +.00000000 +00000-0 +61390-4 0 00002
2 59691 43.0048 349.6471 0001274 255.3986 104.6725 15.27578582 02
| Epoch (UTC): | 25 May 2026 13:26:49 |
| Eccentricity: | 0.0001274 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.6471° |
| argument of perigee: | 255.3986° |
| revolutions per day: | 15.27578582 |
| mean anomaly at epoch: | 104.6725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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