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 26070.59670175 +.00000000 +00000-0 +12832-3 0 00006
2 16615 98.2230 88.1231 0010658 317.7056 155.3285 14.33293907 07
| Epoch (UTC): | 11 March 2026 14:19:15 |
| Eccentricity: | 0.0010658 |
| inclination: | 98.2230° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 88.1231° |
| argument of perigee: | 317.7056° |
| revolutions per day: | 14.33293907 |
| mean anomaly at epoch: | 155.3285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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