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 27717U 26106.72610647 +.00000000 +00000-0 -42219-2 0 00006
2 27717 1.8009 275.7130 7084415 304.8699 325.1370 2.22468914 06
| Epoch (UTC): | 16 April 2026 17:25:35 |
| Eccentricity: | 0.7084415 |
| inclination: | 1.8009° |
| perigee height: | 849 km |
| apogee height: | 35969 km |
| right ascension of ascending node: | 275.7130° |
| argument of perigee: | 304.8699° |
| revolutions per day: | 2.22468914 |
| mean anomaly at epoch: | 325.1370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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