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 26106.85646821 +.00000000 +00000-0 +77041-4 0 00003
2 27607 64.5523 318.7220 0075550 273.6270 85.6198 14.82910703 03
| Epoch (UTC): | 16 April 2026 20:33:18 |
| Eccentricity: | 0.0075550 |
| inclination: | 64.5523° |
| perigee height: | 567 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 318.7220° |
| argument of perigee: | 273.6270° |
| revolutions per day: | 14.82910703 |
| mean anomaly at epoch: | 85.6198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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