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 00047U 26128.18063581 +.00000000 +00000-0 +64220-4 0 00003
2 00047 66.6628 154.0945 0217027 169.2696 191.3155 14.45277233 06
| Epoch (UTC): | 08 May 2026 04:20:06 |
| Eccentricity: | 0.0217027 |
| inclination: | 66.6628° |
| perigee height: | 587 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 154.0945° |
| argument of perigee: | 169.2696° |
| revolutions per day: | 14.45277233 |
| mean anomaly at epoch: | 191.3155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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