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 66351U 26145.51813521 +.00000000 +00000-0 +41711-3 0 00005
2 66351 53.1602 235.2255 0001412 95.1285 264.9878 15.31712995 09
| Epoch (UTC): | 25 May 2026 12:26:06 |
| Eccentricity: | 0.0001412 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 235.2255° |
| argument of perigee: | 95.1285° |
| revolutions per day: | 15.31712995 |
| mean anomaly at epoch: | 264.9878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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