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 63779U 26145.55782323 +.00000000 +00000-0 +55809-3 0 00008
2 63779 43.0025 338.8187 0001154 266.9209 93.1510 15.27588701 04
| Epoch (UTC): | 25 May 2026 13:23:15 |
| Eccentricity: | 0.0001154 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.8187° |
| argument of perigee: | 266.9209° |
| revolutions per day: | 15.27588701 |
| mean anomaly at epoch: | 93.1510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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