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 36110U 26150.62220669 +.00000000 +00000-0 +98984-4 0 00003
2 36110 98.0094 36.5960 0026017 95.5461 264.8718 14.77989763 05
| Epoch (UTC): | 30 May 2026 14:55:58 |
| Eccentricity: | 0.0026017 |
| inclination: | 98.0094° |
| perigee height: | 617 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 36.5960° |
| argument of perigee: | 95.5461° |
| revolutions per day: | 14.77989763 |
| mean anomaly at epoch: | 264.8718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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