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 26103.78189948 +.00000000 +00000-0 +15000-3 0 00007
2 26092 100.2121 116.9628 0030998 329.9195 30.0211 14.48739345 03
| Epoch (UTC): | 13 April 2026 18:45:56 |
| Eccentricity: | 0.0030998 |
| inclination: | 100.2121° |
| perigee height: | 708 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 116.9628° |
| argument of perigee: | 329.9195° |
| revolutions per day: | 14.48739345 |
| mean anomaly at epoch: | 30.0211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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