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 39239U 26145.56093000 +.00000000 +00000-0 +42367-4 0 00006
2 39239 63.3840 148.6023 0424362 11.7576 349.2991 13.45501914 04
| Epoch (UTC): | 25 May 2026 13:27:44 |
| Eccentricity: | 0.0424362 |
| inclination: | 63.3840° |
| perigee height: | 772 km |
| apogee height: | 1406 km |
| right ascension of ascending node: | 148.6023° |
| argument of perigee: | 11.7576° |
| revolutions per day: | 13.45501914 |
| mean anomaly at epoch: | 349.2991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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