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 27646U 26066.03175514 +.00000000 +00000-0 +31254-3 0 00002
2 27646 49.5192 269.5245 5411389 123.6493 303.6649 4.61717262 06
| Epoch (UTC): | 07 March 2026 00:45:43 |
| Eccentricity: | 0.5411389 |
| inclination: | 49.5192° |
| perigee height: | 612 km |
| apogee height: | 17100 km |
| right ascension of ascending node: | 269.5245° |
| argument of perigee: | 123.6493° |
| revolutions per day: | 4.61717262 |
| mean anomaly at epoch: | 303.6649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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