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 27845U 26039.02410750 +.00000000 +00000-0 +25893-3 0 00008
2 27845 98.6669 49.4657 0007996 213.0714 146.9966 14.24826753 09
| Epoch (UTC): | 08 February 2026 00:34:42 |
| Eccentricity: | 0.0007996 |
| inclination: | 98.6669° |
| perigee height: | 803 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 49.4657° |
| argument of perigee: | 213.0714° |
| revolutions per day: | 14.24826753 |
| mean anomaly at epoch: | 146.9966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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