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 50844U 26145.56973292 +.00000000 +00000-0 +61412-5 0 00004
2 50844 53.2117 193.9956 0001426 87.2014 272.9141 15.08832365 06
| Epoch (UTC): | 25 May 2026 13:40:24 |
| Eccentricity: | 0.0001426 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 193.9956° |
| argument of perigee: | 87.2014° |
| revolutions per day: | 15.08832365 |
| mean anomaly at epoch: | 272.9141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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