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 39266U 26099.87942061 +.00000000 +00000-0 +68386-3 0 00006
2 39266 80.9291 73.6225 0104598 57.8419 303.2941 15.86684571 06
| Epoch (UTC): | 09 April 2026 21:06:21 |
| Eccentricity: | 0.0104598 |
| inclination: | 80.9291° |
| perigee height: | 242 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 73.6225° |
| argument of perigee: | 57.8419° |
| revolutions per day: | 15.86684571 |
| mean anomaly at epoch: | 303.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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