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 51956U 26145.60411054 +.00000000 +00000-0 +26155-5 0 00002
2 51956 53.1603 15.9178 0001202 92.6440 267.4699 15.31693502 05
| Epoch (UTC): | 25 May 2026 14:29:55 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 15.9178° |
| argument of perigee: | 92.6440° |
| revolutions per day: | 15.31693502 |
| mean anomaly at epoch: | 267.4699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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