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 26072.92313220 +.00000000 +00000-0 +11137-3 0 00001
2 10967 108.0101 134.3832 0002378 284.3042 75.7840 14.46163930 01
| Epoch (UTC): | 13 March 2026 22:09:18 |
| Eccentricity: | 0.0002378 |
| inclination: | 108.0101° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 134.3832° |
| argument of perigee: | 284.3042° |
| revolutions per day: | 14.46163930 |
| mean anomaly at epoch: | 75.7840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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