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 26072.46172483 +.00000000 +00000-0 +26508-3 0 00001
2 27607 64.5526 65.1060 0075301 280.0120 79.2494 14.82801116 06
| Epoch (UTC): | 13 March 2026 11:04:53 |
| Eccentricity: | 0.0075301 |
| inclination: | 64.5526° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 65.1060° |
| argument of perigee: | 280.0120° |
| revolutions per day: | 14.82801116 |
| mean anomaly at epoch: | 79.2494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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