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 51867U 26145.40136705 +.00000000 +00000-0 +12211-4 0 00005
2 51867 53.2128 24.7493 0001368 108.2964 251.8178 15.08838445 05
| Epoch (UTC): | 25 May 2026 09:37:58 |
| Eccentricity: | 0.0001368 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 24.7493° |
| argument of perigee: | 108.2964° |
| revolutions per day: | 15.08838445 |
| mean anomaly at epoch: | 251.8178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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