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 62240U 26145.61740507 +.00000000 +00000-0 +12742-3 0 00004
2 62240 89.0080 18.6354 0013745 261.9632 98.0001 14.25512185 09
| Epoch (UTC): | 25 May 2026 14:49:03 |
| Eccentricity: | 0.0013745 |
| inclination: | 89.0080° |
| perigee height: | 797 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 18.6354° |
| argument of perigee: | 261.9632° |
| revolutions per day: | 14.25512185 |
| mean anomaly at epoch: | 98.0001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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