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 14781U 26038.93265794 +.00000000 +00000-0 +22116-3 0 00003
2 14781 97.7900 6.1091 0006077 247.6082 112.4493 14.90394435 07
| Epoch (UTC): | 07 February 2026 22:23:01 |
| Eccentricity: | 0.0006077 |
| inclination: | 97.7900° |
| perigee height: | 592 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 6.1091° |
| argument of perigee: | 247.6082° |
| revolutions per day: | 14.90394435 |
| mean anomaly at epoch: | 112.4493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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