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 66540U 26145.55281044 +.00000000 +00000-0 +22162-3 0 00007
2 66540 43.0039 204.2832 0001788 273.6452 86.4195 15.27554180 07
| Epoch (UTC): | 25 May 2026 13:16:02 |
| Eccentricity: | 0.0001788 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.2832° |
| argument of perigee: | 273.6452° |
| revolutions per day: | 15.27554180 |
| mean anomaly at epoch: | 86.4195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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