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 16262U 26071.71671172 +.00000000 +00000-0 +46421-3 0 00008
2 16262 82.4604 318.4506 0005320 6.5479 353.5841 15.50801035 08
| Epoch (UTC): | 12 March 2026 17:12:03 |
| Eccentricity: | 0.0005320 |
| inclination: | 82.4604° |
| perigee height: | 411 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 318.4506° |
| argument of perigee: | 6.5479° |
| revolutions per day: | 15.50801035 |
| mean anomaly at epoch: | 353.5841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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