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 27386U 26065.29547954 +.00000000 +00000-0 +76885-4 0 00001
2 27386 98.3724 18.9737 0001329 84.3919 85.2665 14.39035489 03
| Epoch (UTC): | 06 March 2026 07:05:29 |
| Eccentricity: | 0.0001329 |
| inclination: | 98.3724° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 18.9737° |
| argument of perigee: | 84.3919° |
| revolutions per day: | 14.39035489 |
| mean anomaly at epoch: | 85.2665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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