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 26072.53937881 +.00000000 +00000-0 +26245-3 0 00001
2 27646 49.5191 265.5204 5410608 127.0713 320.5155 4.61718168 08
| Epoch (UTC): | 13 March 2026 12:56:42 |
| Eccentricity: | 0.5410608 |
| inclination: | 49.5191° |
| perigee height: | 613 km |
| apogee height: | 17099 km |
| right ascension of ascending node: | 265.5204° |
| argument of perigee: | 127.0713° |
| revolutions per day: | 4.61718168 |
| mean anomaly at epoch: | 320.5155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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