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 26069.42675395 +.00000000 +00000-0 +28307-3 0 00002
2 27607 64.5525 74.4926 0075267 280.5829 78.6805 14.82787545 09
| Epoch (UTC): | 10 March 2026 10:14:31 |
| Eccentricity: | 0.0075267 |
| inclination: | 64.5525° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 74.4926° |
| argument of perigee: | 280.5829° |
| revolutions per day: | 14.82787545 |
| mean anomaly at epoch: | 78.6805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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