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 62268U 26145.18125433 +.00000000 +00000-0 +17316-2 0 00002
2 62268 42.9994 315.4355 0001296 39.7385 320.3578 15.70891714 03
| Epoch (UTC): | 25 May 2026 04:21:00 |
| Eccentricity: | 0.0001296 |
| inclination: | 42.9994° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 315.4355° |
| argument of perigee: | 39.7385° |
| revolutions per day: | 15.70891714 |
| mean anomaly at epoch: | 320.3578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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