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 10677U 26037.95782089 +.00000000 +00000-0 +15612-3 0 00008
2 10677 74.0357 224.9370 0015760 243.9587 115.9946 14.41686843 03
| Epoch (UTC): | 06 February 2026 22:59:15 |
| Eccentricity: | 0.0015760 |
| inclination: | 74.0357° |
| perigee height: | 742 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 224.9370° |
| argument of perigee: | 243.9587° |
| revolutions per day: | 14.41686843 |
| mean anomaly at epoch: | 115.9946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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