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 50846U 26145.37838431 +.00000000 +00000-0 -30759-4 0 00000
2 50846 53.2110 194.9689 0001417 83.2871 276.8282 15.08839867 05
| Epoch (UTC): | 25 May 2026 09:04:52 |
| Eccentricity: | 0.0001417 |
| inclination: | 53.2110° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.9689° |
| argument of perigee: | 83.2871° |
| revolutions per day: | 15.08839867 |
| mean anomaly at epoch: | 276.8282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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