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 66036U 26145.47414023 +.00000000 +00000-0 +17455-3 0 00002
2 66036 89.0026 45.4096 0002100 73.6446 286.4936 13.51006244 03
| Epoch (UTC): | 25 May 2026 11:22:45 |
| Eccentricity: | 0.0002100 |
| inclination: | 89.0026° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4096° |
| argument of perigee: | 73.6446° |
| revolutions per day: | 13.51006244 |
| mean anomaly at epoch: | 286.4936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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