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 10461U 26069.38018597 +.00000000 +00000-0 +73841-4 0 00006
2 10461 82.9533 166.1585 0032491 222.5629 212.8043 13.77136763 07
| Epoch (UTC): | 10 March 2026 09:07:28 |
| Eccentricity: | 0.0032491 |
| inclination: | 82.9533° |
| perigee height: | 950 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 166.1585° |
| argument of perigee: | 222.5629° |
| revolutions per day: | 13.77136763 |
| mean anomaly at epoch: | 212.8043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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