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 26040.30198036 +.00000000 +00000-0 +79890-4 0 00008
2 27610 64.5591 173.6101 0266876 110.6570 269.4101 14.29500848 06
| Epoch (UTC): | 09 February 2026 07:14:51 |
| Eccentricity: | 0.0266876 |
| inclination: | 64.5591° |
| perigee height: | 602 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 173.6101° |
| argument of perigee: | 110.6570° |
| revolutions per day: | 14.29500848 |
| mean anomaly at epoch: | 269.4101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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