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 65666U 26145.37921821 +.00000000 +00000-0 +57105-3 0 00004
2 65666 97.4484 189.3195 0002525 115.2166 244.9323 15.05654102 05
| Epoch (UTC): | 25 May 2026 09:06:04 |
| Eccentricity: | 0.0002525 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.3195° |
| argument of perigee: | 115.2166° |
| revolutions per day: | 15.05654102 |
| mean anomaly at epoch: | 244.9323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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