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 51996U 26145.10236782 +.00000000 +00000-0 +38117-4 0 00004
2 51996 53.2133 36.0895 0001165 81.6080 278.5044 15.08836208 07
| Epoch (UTC): | 25 May 2026 02:27:24 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 36.0895° |
| argument of perigee: | 81.6080° |
| revolutions per day: | 15.08836208 |
| mean anomaly at epoch: | 278.5044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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