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 10967U 26066.07508735 +.00000000 +00000-0 +10647-3 0 00002
2 10967 108.0115 120.0133 0002279 285.9434 74.1460 14.46157299 06
| Epoch (UTC): | 07 March 2026 01:48:07 |
| Eccentricity: | 0.0002279 |
| inclination: | 108.0115° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 120.0133° |
| argument of perigee: | 285.9434° |
| revolutions per day: | 14.46157299 |
| mean anomaly at epoch: | 74.1460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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