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 66963U 26145.50114309 +.00000000 +00000-0 +66647-3 0 00006
2 66963 43.0013 309.7557 0001303 280.2892 79.7813 15.27580771 05
| Epoch (UTC): | 25 May 2026 12:01:38 |
| Eccentricity: | 0.0001303 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7557° |
| argument of perigee: | 280.2892° |
| revolutions per day: | 15.27580771 |
| mean anomaly at epoch: | 79.7813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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