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 26075.85676623 +.00000000 +00000-0 +16474-3 0 00002
2 14781 97.7958 42.5319 0008850 122.9378 237.2692 14.90532274 03
| Epoch (UTC): | 16 March 2026 20:33:44 |
| Eccentricity: | 0.0008850 |
| inclination: | 97.7958° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 42.5319° |
| argument of perigee: | 122.9378° |
| revolutions per day: | 14.90532274 |
| mean anomaly at epoch: | 237.2692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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