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 66136U 26145.44077624 +.00000000 +00000-0 +35106-3 0 00005
2 66136 53.1616 42.9613 0001559 96.3217 263.7961 15.30208820 02
| Epoch (UTC): | 25 May 2026 10:34:43 |
| Eccentricity: | 0.0001559 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.9613° |
| argument of perigee: | 96.3217° |
| revolutions per day: | 15.30208820 |
| mean anomaly at epoch: | 263.7961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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