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 26021.45834118 +.00000000 +00000-0 +22943-3 0 00004
2 10967 108.0166 26.3764 0001216 283.0739 77.0271 14.46111778 01
| Epoch (UTC): | 21 January 2026 11:00:00 |
| Eccentricity: | 0.0001216 |
| inclination: | 108.0166° |
| perigee height: | 738 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 26.3764° |
| argument of perigee: | 283.0739° |
| revolutions per day: | 14.46111778 |
| mean anomaly at epoch: | 77.0271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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