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 66884U 26145.37028263 +.00000000 +00000-0 +63375-3 0 00001
2 66884 53.1588 28.0408 0000602 58.6764 301.4297 15.34407838 09
| Epoch (UTC): | 25 May 2026 08:53:12 |
| Eccentricity: | 0.0000602 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 28.0408° |
| argument of perigee: | 58.6764° |
| revolutions per day: | 15.34407838 |
| mean anomaly at epoch: | 301.4297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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