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 55939U 26145.54831691 +.00000000 +00000-0 +80110-4 0 00003
2 55939 69.9998 90.6402 0003417 263.1655 96.9115 14.98316568 09
| Epoch (UTC): | 25 May 2026 13:09:34 |
| Eccentricity: | 0.0003417 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 90.6402° |
| argument of perigee: | 263.1655° |
| revolutions per day: | 14.98316568 |
| mean anomaly at epoch: | 96.9115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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