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 66769U 26145.45366169 +.00000000 +00000-0 +19228-3 0 00000
2 66769 97.4212 219.6270 0000909 50.0734 310.0581 15.20257857 05
| Epoch (UTC): | 25 May 2026 10:53:16 |
| Eccentricity: | 0.0000909 |
| inclination: | 97.4212° |
| perigee height: | 504 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.6270° |
| argument of perigee: | 50.0734° |
| revolutions per day: | 15.20257857 |
| mean anomaly at epoch: | 310.0581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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