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 55439U 26145.64219758 +.00000000 +00000-0 -18488-4 0 00003
2 55439 69.9989 270.4999 0002864 267.8764 92.2067 14.98330093 04
| Epoch (UTC): | 25 May 2026 15:24:45 |
| Eccentricity: | 0.0002864 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.4999° |
| argument of perigee: | 267.8764° |
| revolutions per day: | 14.98330093 |
| mean anomaly at epoch: | 92.2067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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