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 62567U 26145.20477074 +.00000000 +00000-0 +53720-3 0 00008
2 62567 43.0006 220.5528 0002520 283.0547 77.0023 15.27590306 00
| Epoch (UTC): | 25 May 2026 04:54:52 |
| Eccentricity: | 0.0002520 |
| inclination: | 43.0006° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 220.5528° |
| argument of perigee: | 283.0547° |
| revolutions per day: | 15.27590306 |
| mean anomaly at epoch: | 77.0023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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