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 39240U 26145.53128339 +.00000000 +00000-0 -57385-4 0 00006
2 39240 63.3850 149.2967 0424469 11.2901 349.7290 13.45469037 02
| Epoch (UTC): | 25 May 2026 12:45:02 |
| Eccentricity: | 0.0424469 |
| inclination: | 63.3850° |
| perigee height: | 772 km |
| apogee height: | 1406 km |
| right ascension of ascending node: | 149.2967° |
| argument of perigee: | 11.2901° |
| revolutions per day: | 13.45469037 |
| mean anomaly at epoch: | 349.7290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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