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 26150.75919301 +.00000000 +00000-0 +53731-3 0 00002
2 26091 100.1802 259.5849 0023916 6.9970 353.1552 14.59893104 04
| Epoch (UTC): | 30 May 2026 18:13:14 |
| Eccentricity: | 0.0023916 |
| inclination: | 100.1802° |
| perigee height: | 677 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 259.5849° |
| argument of perigee: | 6.9970° |
| revolutions per day: | 14.59893104 |
| mean anomaly at epoch: | 353.1552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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