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 51855U 26145.40777753 +.00000000 +00000-0 +13062-3 0 00000
2 51855 53.2142 34.6375 0001500 84.1068 276.0096 15.08857516 00
| Epoch (UTC): | 25 May 2026 09:47:11 |
| Eccentricity: | 0.0001500 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.6375° |
| argument of perigee: | 84.1068° |
| revolutions per day: | 15.08857516 |
| mean anomaly at epoch: | 276.0096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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