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 25159U 26106.24254545 +.00000000 +00000-0 +23175-3 0 00002
2 25159 107.9610 41.9525 0038860 73.7453 286.7957 14.35613294 00
| Epoch (UTC): | 16 April 2026 05:49:15 |
| Eccentricity: | 0.0038860 |
| inclination: | 107.9610° |
| perigee height: | 745 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 41.9525° |
| argument of perigee: | 73.7453° |
| revolutions per day: | 14.35613294 |
| mean anomaly at epoch: | 286.7957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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