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 62239U 26145.62322385 +.00000000 +00000-0 +14732-3 0 00004
2 62239 89.0101 24.7753 0016581 81.5206 278.7823 13.51009808 06
| Epoch (UTC): | 25 May 2026 14:57:26 |
| Eccentricity: | 0.0016581 |
| inclination: | 89.0101° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 24.7753° |
| argument of perigee: | 81.5206° |
| revolutions per day: | 13.51009808 |
| mean anomaly at epoch: | 278.7823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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