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 26039.60022866 +.00000000 +00000-0 +13051-3 0 00005
2 16615 98.2245 58.6736 0012477 49.8750 59.5268 14.33272172 07
| Epoch (UTC): | 08 February 2026 14:24:19 |
| Eccentricity: | 0.0012477 |
| inclination: | 98.2245° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 58.6736° |
| argument of perigee: | 49.8750° |
| revolutions per day: | 14.33272172 |
| mean anomaly at epoch: | 59.5268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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