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 50486U 26145.28457758 +.00000000 +00000-0 -46658-4 0 00004
2 50486 87.9160 340.0151 0002339 96.8463 263.2936 13.18687938 08
| Epoch (UTC): | 25 May 2026 06:49:47 |
| Eccentricity: | 0.0002339 |
| inclination: | 87.9160° |
| perigee height: | 1188 km |
| apogee height: | 1192 km |
| right ascension of ascending node: | 340.0151° |
| argument of perigee: | 96.8463° |
| revolutions per day: | 13.18687938 |
| mean anomaly at epoch: | 263.2936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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