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 50005U 26145.26115240 +.00000000 +00000-0 +00000-0 0 00002
2 50005 0.7444 86.4477 0001931 220.8094 200.5670 1.00271131 02
| Epoch (UTC): | 25 May 2026 06:16:03 |
| Eccentricity: | 0.0001931 |
| inclination: | 0.7444° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 86.4477° |
| argument of perigee: | 220.8094° |
| revolutions per day: | 1.00271131 |
| mean anomaly at epoch: | 200.5670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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