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 09841U 26053.86649836 +.00000000 +00000-0 +67111-5 0 00002
2 09841 65.7649 10.7760 1735821 290.1339 52.1563 10.73916544 08
| Epoch (UTC): | 22 February 2026 20:47:45 |
| Eccentricity: | 0.1735821 |
| inclination: | 65.7649° |
| perigee height: | 794 km |
| apogee height: | 3806 km |
| right ascension of ascending node: | 10.7760° |
| argument of perigee: | 290.1339° |
| revolutions per day: | 10.73916544 |
| mean anomaly at epoch: | 52.1563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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