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 26088.22433492 +.00000000 +00000-0 +86091-4 0 00007
2 16682 74.0226 93.0694 0013984 8.4695 72.4192 14.37315966 04
| Epoch (UTC): | 29 March 2026 05:23:02 |
| Eccentricity: | 0.0013984 |
| inclination: | 74.0226° |
| perigee height: | 757 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 93.0694° |
| argument of perigee: | 8.4695° |
| revolutions per day: | 14.37315966 |
| mean anomaly at epoch: | 72.4192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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