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 26073.40870728 +.00000000 +00000-0 +44587-4 0 00005
2 27610 64.5581 79.5062 0265792 101.2734 4.8383 14.29512665 02
| Epoch (UTC): | 14 March 2026 09:48:32 |
| Eccentricity: | 0.0265792 |
| inclination: | 64.5581° |
| perigee height: | 603 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 79.5062° |
| argument of perigee: | 101.2734° |
| revolutions per day: | 14.29512665 |
| mean anomaly at epoch: | 4.8383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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