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 25544U 26017.85314278 +.00000000 +00000-0 +24462-3 0 00008
2 25544 51.6334 323.6922 0007803 29.9146 330.2287 15.49362465 00
| Epoch (UTC): | 17 January 2026 20:28:31 |
| Eccentricity: | 0.0007803 |
| inclination: | 51.6334° |
| perigee height: | 413 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 323.6922° |
| argument of perigee: | 29.9146° |
| revolutions per day: | 15.49362465 |
| mean anomaly at epoch: | 330.2287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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