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 16263U 26073.54705558 +.00000000 +00000-0 +69516-4 0 00009
2 16263 82.5065 356.4956 0017569 264.0735 269.1267 14.85525195 07
| Epoch (UTC): | 14 March 2026 13:07:45 |
| Eccentricity: | 0.0017569 |
| inclination: | 82.5065° |
| perigee height: | 600 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 356.4956° |
| argument of perigee: | 264.0735° |
| revolutions per day: | 14.85525195 |
| mean anomaly at epoch: | 269.1267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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