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 26041.96404705 +.00000000 +00000-0 +12188-3 0 00003
2 16615 98.2243 60.9195 0012369 43.3010 15.8362 14.33273819 07
| Epoch (UTC): | 10 February 2026 23:08:13 |
| Eccentricity: | 0.0012369 |
| inclination: | 98.2243° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 60.9195° |
| argument of perigee: | 43.3010° |
| revolutions per day: | 14.33273819 |
| mean anomaly at epoch: | 15.8362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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