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 55311U 26145.42407531 +.00000000 +00000-0 +43737-4 0 00000
2 55311 69.9983 171.0886 0003788 269.1049 90.9677 14.98339144 03
| Epoch (UTC): | 25 May 2026 10:10:40 |
| Eccentricity: | 0.0003788 |
| inclination: | 69.9983° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 171.0886° |
| argument of perigee: | 269.1049° |
| revolutions per day: | 14.98339144 |
| mean anomaly at epoch: | 90.9677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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