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 62417U 26145.46540773 +.00000000 +00000-0 +16119-2 0 00007
2 62417 42.9997 65.0454 0002457 281.3400 78.7192 15.70913213 08
| Epoch (UTC): | 25 May 2026 11:10:11 |
| Eccentricity: | 0.0002457 |
| inclination: | 42.9997° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 65.0454° |
| argument of perigee: | 281.3400° |
| revolutions per day: | 15.70913213 |
| mean anomaly at epoch: | 78.7192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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