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 26103.96682964 +.00000000 +00000-0 +42606-4 0 00009
2 09841 65.7611 296.6218 1735297 275.9414 64.7292 10.73914886 07
| Epoch (UTC): | 13 April 2026 23:12:14 |
| Eccentricity: | 0.1735297 |
| inclination: | 65.7611° |
| perigee height: | 794 km |
| apogee height: | 3806 km |
| right ascension of ascending node: | 296.6218° |
| argument of perigee: | 275.9414° |
| revolutions per day: | 10.73914886 |
| mean anomaly at epoch: | 64.7292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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