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 16182U 26038.91578264 +.00000000 +00000-0 -68941-7 0 00008
2 16182 71.0016 203.2320 0009584 294.5187 178.7757 14.16596400 07
| Epoch (UTC): | 07 February 2026 21:58:43 |
| Eccentricity: | 0.0009584 |
| inclination: | 71.0016° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 203.2320° |
| argument of perigee: | 294.5187° |
| revolutions per day: | 14.16596400 |
| mean anomaly at epoch: | 178.7757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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