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 62522U 26145.52344457 +.00000000 +00000-0 +16534-2 0 00003
2 62522 42.9972 327.4932 0001801 277.3631 82.7032 15.70913948 00
| Epoch (UTC): | 25 May 2026 12:33:45 |
| Eccentricity: | 0.0001801 |
| inclination: | 42.9972° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 327.4932° |
| argument of perigee: | 277.3631° |
| revolutions per day: | 15.70913948 |
| mean anomaly at epoch: | 82.7032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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