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 66569U 26145.64533233 +.00000000 +00000-0 +61248-3 0 00006
2 66569 43.0018 272.0650 0000704 265.9512 94.1260 15.27589048 04
| Epoch (UTC): | 25 May 2026 15:29:16 |
| Eccentricity: | 0.0000704 |
| inclination: | 43.0018° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.0650° |
| argument of perigee: | 265.9512° |
| revolutions per day: | 15.27589048 |
| mean anomaly at epoch: | 94.1260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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