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 62279U 26145.48957692 +.00000000 +00000-0 +18293-2 0 00002
2 62279 42.9984 314.3314 0002210 273.8972 86.1643 15.70894208 08
| Epoch (UTC): | 25 May 2026 11:44:59 |
| Eccentricity: | 0.0002210 |
| inclination: | 42.9984° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 314.3314° |
| argument of perigee: | 273.8972° |
| revolutions per day: | 15.70894208 |
| mean anomaly at epoch: | 86.1643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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