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 62039U 26145.45550311 +.00000000 +00000-0 +36768-3 0 00008
2 62039 42.9997 182.9893 0001551 273.2312 86.8362 15.27592816 03
| Epoch (UTC): | 25 May 2026 10:55:55 |
| Eccentricity: | 0.0001551 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.9893° |
| argument of perigee: | 273.2312° |
| revolutions per day: | 15.27592816 |
| mean anomaly at epoch: | 86.8362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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