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 26550U 26158.76838691 +.00000000 +00000-0 +60861-4 0 00006
2 26550 64.5633 344.1867 0513108 32.1069 331.0171 13.82099778 09
| Epoch (UTC): | 07 June 2026 18:26:28 |
| Eccentricity: | 0.0513108 |
| inclination: | 64.5633° |
| perigee height: | 580 km |
| apogee height: | 1333 km |
| right ascension of ascending node: | 344.1867° |
| argument of perigee: | 32.1069° |
| revolutions per day: | 13.82099778 |
| mean anomaly at epoch: | 331.0171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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