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 16615U 26022.50678953 +.00000000 +00000-0 +20499-3 0 00004
2 16615 98.2249 42.4338 0012800 96.3778 66.1063 14.33255785 05
| Epoch (UTC): | 22 January 2026 12:09:46 |
| Eccentricity: | 0.0012800 |
| inclination: | 98.2249° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 42.4338° |
| argument of perigee: | 96.3778° |
| revolutions per day: | 14.33255785 |
| mean anomaly at epoch: | 66.1063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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