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 68177U 26145.43780252 +.00000000 +00000-0 -51605-2 0 00001
2 68177 53.1576 269.5711 0008007 308.8647 51.1643 15.41586355 03
| Epoch (UTC): | 25 May 2026 10:30:26 |
| Eccentricity: | 0.0008007 |
| inclination: | 53.1576° |
| perigee height: | 436 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 269.5711° |
| argument of perigee: | 308.8647° |
| revolutions per day: | 15.41586355 |
| mean anomaly at epoch: | 51.1643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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