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 16882U 26088.13354080 +.00000000 +00000-0 +54121-4 0 00003
2 16882 82.5170 108.3936 0017300 267.6788 156.6193 14.85659607 07
| Epoch (UTC): | 29 March 2026 03:12:17 |
| Eccentricity: | 0.0017300 |
| inclination: | 82.5170° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 108.3936° |
| argument of perigee: | 267.6788° |
| revolutions per day: | 14.85659607 |
| mean anomaly at epoch: | 156.6193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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