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 26064.24074006 +.00000000 +00000-0 +95002-4 0 00002
2 16263 82.5060 5.2586 0017735 297.5460 177.4753 14.85512265 06
| Epoch (UTC): | 05 March 2026 05:46:39 |
| Eccentricity: | 0.0017735 |
| inclination: | 82.5060° |
| perigee height: | 600 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 5.2586° |
| argument of perigee: | 297.5460° |
| revolutions per day: | 14.85512265 |
| mean anomaly at epoch: | 177.4753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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