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 55667U 26145.50518638 +.00000000 +00000-0 -73801-5 0 00001
2 55667 69.9990 330.6612 0002816 270.0175 90.0661 14.98330405 02
| Epoch (UTC): | 25 May 2026 12:07:28 |
| Eccentricity: | 0.0002816 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.6612° |
| argument of perigee: | 270.0175° |
| revolutions per day: | 14.98330405 |
| mean anomaly at epoch: | 90.0661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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