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 26158.74174166 +.00000000 +00000-0 +56382-4 0 00007
2 16263 82.5027 276.2275 0018631 347.0640 127.1303 14.85594140 06
| Epoch (UTC): | 07 June 2026 17:48:06 |
| Eccentricity: | 0.0018631 |
| inclination: | 82.5027° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 276.2275° |
| argument of perigee: | 347.0640° |
| revolutions per day: | 14.85594140 |
| mean anomaly at epoch: | 127.1303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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