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 27610U 26064.52737203 +.00000000 +00000-0 +53015-4 0 00004
2 27610 64.5584 104.7528 0265973 103.7844 19.1566 14.29509811 04
| Epoch (UTC): | 05 March 2026 12:39:24 |
| Eccentricity: | 0.0265973 |
| inclination: | 64.5584° |
| perigee height: | 603 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 104.7528° |
| argument of perigee: | 103.7844° |
| revolutions per day: | 14.29509811 |
| mean anomaly at epoch: | 19.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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