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 66740U 26145.44863106 +.00000000 +00000-0 +26767-3 0 00007
2 66740 97.4212 219.4810 0004723 83.5729 276.6044 15.19952291 08
| Epoch (UTC): | 25 May 2026 10:46:01 |
| Eccentricity: | 0.0004723 |
| inclination: | 97.4212° |
| perigee height: | 503 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.4810° |
| argument of perigee: | 83.5729° |
| revolutions per day: | 15.19952291 |
| mean anomaly at epoch: | 276.6044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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