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 55312U 26145.39484274 +.00000000 +00000-0 +41621-4 0 00006
2 55312 69.9986 170.8743 0003647 266.5106 93.5636 14.98331693 00
| Epoch (UTC): | 25 May 2026 09:28:34 |
| Eccentricity: | 0.0003647 |
| inclination: | 69.9986° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.8743° |
| argument of perigee: | 266.5106° |
| revolutions per day: | 14.98331693 |
| mean anomaly at epoch: | 93.5636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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