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 26106.76053743 +.00000000 +00000-0 -11656-4 0 00009
2 09841 65.7608 292.4859 1735238 275.1518 65.4597 10.73914914 08
| Epoch (UTC): | 16 April 2026 18:15:10 |
| Eccentricity: | 0.1735238 |
| inclination: | 65.7608° |
| perigee height: | 794 km |
| apogee height: | 3806 km |
| right ascension of ascending node: | 292.4859° |
| argument of perigee: | 275.1518° |
| revolutions per day: | 10.73914914 |
| mean anomaly at epoch: | 65.4597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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