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 66878U 26145.09514465 +.00000000 +00000-0 -22462-3 0 00000
2 66878 53.1597 29.1694 0001395 82.9789 277.1370 15.30165339 02
| Epoch (UTC): | 25 May 2026 02:17:00 |
| Eccentricity: | 0.0001395 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.1694° |
| argument of perigee: | 82.9789° |
| revolutions per day: | 15.30165339 |
| mean anomaly at epoch: | 277.1370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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