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 51109U 26145.43448321 +.00000000 +00000-0 +99420-5 0 00005
2 51109 53.2120 304.5516 0001085 76.8109 283.3004 15.08838299 03
| Epoch (UTC): | 25 May 2026 10:25:39 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 304.5516° |
| argument of perigee: | 76.8109° |
| revolutions per day: | 15.08838299 |
| mean anomaly at epoch: | 283.3004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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