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 62577U 26145.63225684 +.00000000 +00000-0 +83853-4 0 00005
2 62577 54.9863 10.4449 0016316 78.6914 281.5875 13.80629637 09
| Epoch (UTC): | 25 May 2026 15:10:26 |
| Eccentricity: | 0.0016316 |
| inclination: | 54.9863° |
| perigee height: | 950 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 10.4449° |
| argument of perigee: | 78.6914° |
| revolutions per day: | 13.80629637 |
| mean anomaly at epoch: | 281.5875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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