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 39012U 26145.51658616 +.00000000 +00000-0 +36065-4 0 00008
2 39012 63.3554 348.5781 0433883 26.7078 335.5595 13.45512170 02
| Epoch (UTC): | 25 May 2026 12:23:53 |
| Eccentricity: | 0.0433883 |
| inclination: | 63.3554° |
| perigee height: | 765 km |
| apogee height: | 1413 km |
| right ascension of ascending node: | 348.5781° |
| argument of perigee: | 26.7078° |
| revolutions per day: | 13.45512170 |
| mean anomaly at epoch: | 335.5595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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