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 20663U 26128.15635087 +.00000000 +00000-0 +11813-3 0 00001
2 20663 62.7872 132.7028 0008023 219.9068 140.1443 15.05953414 06
| Epoch (UTC): | 08 May 2026 03:45:08 |
| Eccentricity: | 0.0008023 |
| inclination: | 62.7872° |
| perigee height: | 543 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 132.7028° |
| argument of perigee: | 219.9068° |
| revolutions per day: | 15.05953414 |
| mean anomaly at epoch: | 140.1443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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