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 26091U 26104.22032235 +.00000000 +00000-0 +27806-3 0 00009
2 26091 100.1753 202.5683 0025077 140.7723 219.5294 14.59725350 01
| Epoch (UTC): | 14 April 2026 05:17:15 |
| Eccentricity: | 0.0025077 |
| inclination: | 100.1753° |
| perigee height: | 676 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 202.5683° |
| argument of perigee: | 140.7723° |
| revolutions per day: | 14.59725350 |
| mean anomaly at epoch: | 219.5294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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