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 60926U 26145.48954330 +.00000000 +00000-0 +94462-5 0 00000
2 60926 53.1565 322.7303 0000525 67.5414 292.5660 15.69714276 07
| Epoch (UTC): | 25 May 2026 11:44:56 |
| Eccentricity: | 0.0000525 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.7303° |
| argument of perigee: | 67.5414° |
| revolutions per day: | 15.69714276 |
| mean anomaly at epoch: | 292.5660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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