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 26020.87208451 +.00000000 +00000-0 +32299-3 0 00007
2 14781 97.7869 348.3082 0006631 321.9851 38.0899 14.90301799 02
| Epoch (UTC): | 20 January 2026 20:55:48 |
| Eccentricity: | 0.0006631 |
| inclination: | 97.7869° |
| perigee height: | 592 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 348.3082° |
| argument of perigee: | 321.9851° |
| revolutions per day: | 14.90301799 |
| mean anomaly at epoch: | 38.0899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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