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 63758U 26145.43462904 +.00000000 +00000-0 +12964-2 0 00006
2 63758 43.0016 189.8136 0002412 259.1798 100.8798 15.70857563 01
| Epoch (UTC): | 25 May 2026 10:25:51 |
| Eccentricity: | 0.0002412 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 189.8136° |
| argument of perigee: | 259.1798° |
| revolutions per day: | 15.70857563 |
| mean anomaly at epoch: | 100.8798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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