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 26160.19727723 +.00000000 +00000-0 +31493-3 0 00006
2 16262 82.4571 225.4898 0004512 38.8614 321.2963 15.54787027 08
| Epoch (UTC): | 09 June 2026 04:44:04 |
| Eccentricity: | 0.0004512 |
| inclination: | 82.4571° |
| perigee height: | 400 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 225.4898° |
| argument of perigee: | 38.8614° |
| revolutions per day: | 15.54787027 |
| mean anomaly at epoch: | 321.2963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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