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 26071.12465845 +.00000000 +00000-0 +10995-3 0 00004
2 10967 108.0105 130.6094 0002363 285.2592 74.8292 14.46162302 01
| Epoch (UTC): | 12 March 2026 02:59:30 |
| Eccentricity: | 0.0002363 |
| inclination: | 108.0105° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 130.6094° |
| argument of perigee: | 285.2592° |
| revolutions per day: | 14.46162302 |
| mean anomaly at epoch: | 74.8292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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