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 51869U 26145.65528854 +.00000000 +00000-0 +30712-4 0 00000
2 51869 53.2117 23.6091 0001555 90.2165 269.9005 15.08838497 04
| Epoch (UTC): | 25 May 2026 15:43:36 |
| Eccentricity: | 0.0001555 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 23.6091° |
| argument of perigee: | 90.2165° |
| revolutions per day: | 15.08838497 |
| mean anomaly at epoch: | 269.9005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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