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 26067.94273873 +.00000000 +00000-0 +13028-3 0 00007
2 10967 108.0110 123.9324 0002295 286.4076 73.6817 14.46159630 02
| Epoch (UTC): | 08 March 2026 22:37:32 |
| Eccentricity: | 0.0002295 |
| inclination: | 108.0110° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 123.9324° |
| argument of perigee: | 286.4076° |
| revolutions per day: | 14.46159630 |
| mean anomaly at epoch: | 73.6817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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