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 26070.23259977 +.00000000 +00000-0 +53311-3 0 00005
2 16262 82.4600 320.0050 0005724 11.5714 348.5668 15.50720749 06
| Epoch (UTC): | 11 March 2026 05:34:56 |
| Eccentricity: | 0.0005724 |
| inclination: | 82.4600° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 320.0050° |
| argument of perigee: | 11.5714° |
| revolutions per day: | 15.50720749 |
| mean anomaly at epoch: | 348.5668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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