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 16682U 26064.64462922 +.00000000 +00000-0 +11979-3 0 00009
2 16682 74.0252 136.4809 0013193 60.1713 100.9946 14.37302373 03
| Epoch (UTC): | 05 March 2026 15:28:15 |
| Eccentricity: | 0.0013193 |
| inclination: | 74.0252° |
| perigee height: | 758 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 136.4809° |
| argument of perigee: | 60.1713° |
| revolutions per day: | 14.37302373 |
| mean anomaly at epoch: | 100.9946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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