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 26159.87437095 +.00000000 +00000-0 +41207-3 0 00004
2 26091 100.1805 270.7575 0023582 339.7393 20.2862 14.59933890 06
| Epoch (UTC): | 08 June 2026 20:59:05 |
| Eccentricity: | 0.0023582 |
| inclination: | 100.1805° |
| perigee height: | 677 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 270.7575° |
| argument of perigee: | 339.7393° |
| revolutions per day: | 14.59933890 |
| mean anomaly at epoch: | 20.2862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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