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 26073.40733627 +.00000000 +00000-0 +11329-3 0 00005
2 10967 108.0100 135.3991 0002394 283.9369 76.1511 14.46164411 07
| Epoch (UTC): | 14 March 2026 09:46:33 |
| Eccentricity: | 0.0002394 |
| inclination: | 108.0100° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 135.3991° |
| argument of perigee: | 283.9369° |
| revolutions per day: | 14.46164411 |
| mean anomaly at epoch: | 76.1511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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