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 26064.20177200 +.00000000 +00000-0 +10670-3 0 00000
2 16682 74.0253 137.2961 0013181 61.1582 329.4588 14.37301874 09
| Epoch (UTC): | 05 March 2026 04:50:33 |
| Eccentricity: | 0.0013181 |
| inclination: | 74.0253° |
| perigee height: | 758 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 137.2961° |
| argument of perigee: | 61.1582° |
| revolutions per day: | 14.37301874 |
| mean anomaly at epoch: | 329.4588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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