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 26039.54166198 +.00000000 +00000-0 -15646-4 0 00008
2 16182 71.0017 201.9143 0009591 293.7352 130.4329 14.16596407 06
| Epoch (UTC): | 08 February 2026 12:59:59 |
| Eccentricity: | 0.0009591 |
| inclination: | 71.0017° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 201.9143° |
| argument of perigee: | 293.7352° |
| revolutions per day: | 14.16596407 |
| mean anomaly at epoch: | 130.4329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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