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 50805U 26145.45750431 +.00000000 +00000-0 -99221-4 0 00006
2 50805 53.2128 174.4952 0000964 69.5618 290.5478 15.08822001 09
| Epoch (UTC): | 25 May 2026 10:58:48 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.4952° |
| argument of perigee: | 69.5618° |
| revolutions per day: | 15.08822001 |
| mean anomaly at epoch: | 290.5478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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