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 27607U 26136.66362443 +.00000000 +00000-0 +90219-4 0 00002
2 27607 64.5521 226.5121 0075629 268.2379 91.0064 14.82976040 03
| Epoch (UTC): | 16 May 2026 15:55:37 |
| Eccentricity: | 0.0075629 |
| inclination: | 64.5521° |
| perigee height: | 567 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 226.5121° |
| argument of perigee: | 268.2379° |
| revolutions per day: | 14.82976040 |
| mean anomaly at epoch: | 91.0064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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