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 55274U 26145.52027088 +.00000000 +00000-0 +50394-4 0 00001
2 55274 69.9990 190.8999 0003685 268.9585 91.1152 14.98329791 09
| Epoch (UTC): | 25 May 2026 12:29:11 |
| Eccentricity: | 0.0003685 |
| inclination: | 69.9990° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.8999° |
| argument of perigee: | 268.9585° |
| revolutions per day: | 14.98329791 |
| mean anomaly at epoch: | 91.1152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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