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 16511U 26071.20349058 +.00000000 +00000-0 +49454-4 0 00004
2 16511 82.9475 13.9309 0024585 13.9369 98.3276 13.75986977 08
| Epoch (UTC): | 12 March 2026 04:53:01 |
| Eccentricity: | 0.0024585 |
| inclination: | 82.9475° |
| perigee height: | 960 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 13.9309° |
| argument of perigee: | 13.9369° |
| revolutions per day: | 13.75986977 |
| mean anomaly at epoch: | 98.3276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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