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 26092U 26087.96623472 +.00000000 +00000-0 +30367-3 0 00006
2 26092 100.2131 97.8609 0031637 15.6010 344.6145 14.48703445 08
| Epoch (UTC): | 28 March 2026 23:11:22 |
| Eccentricity: | 0.0031637 |
| inclination: | 100.2131° |
| perigee height: | 707 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 97.8609° |
| argument of perigee: | 15.6010° |
| revolutions per day: | 14.48703445 |
| mean anomaly at epoch: | 344.6145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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