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 62214U 26145.43190088 +.00000000 +00000-0 +46935-3 0 00009
2 62214 43.0001 197.6889 0002082 273.5303 86.5311 15.27585529 01
| Epoch (UTC): | 25 May 2026 10:21:56 |
| Eccentricity: | 0.0002082 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.6889° |
| argument of perigee: | 273.5303° |
| revolutions per day: | 15.27585529 |
| mean anomaly at epoch: | 86.5311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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