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 26386U 26087.92453913 +.00000000 +00000-0 +22517-3 0 00007
2 26386 97.7534 78.0103 0010363 157.8497 202.3162 14.74706308 01
| Epoch (UTC): | 28 March 2026 22:11:20 |
| Eccentricity: | 0.0010363 |
| inclination: | 97.7534° |
| perigee height: | 639 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 78.0103° |
| argument of perigee: | 157.8497° |
| revolutions per day: | 14.74706308 |
| mean anomaly at epoch: | 202.3162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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