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 50993U 26145.54521076 +.00000000 +00000-0 +17211-3 0 00002
2 50993 97.2850 203.6317 0009061 79.0837 281.1423 15.30188113 03
| Epoch (UTC): | 25 May 2026 13:05:06 |
| Eccentricity: | 0.0009061 |
| inclination: | 97.2850° |
| perigee height: | 469 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 203.6317° |
| argument of perigee: | 79.0837° |
| revolutions per day: | 15.30188113 |
| mean anomaly at epoch: | 281.1423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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