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 50498U 26145.24665639 +.00000000 +00000-0 +23740-3 0 00007
2 50498 87.9168 340.0111 0002544 89.4470 270.6953 13.18687539 07
| Epoch (UTC): | 25 May 2026 05:55:11 |
| Eccentricity: | 0.0002544 |
| inclination: | 87.9168° |
| perigee height: | 1188 km |
| apogee height: | 1192 km |
| right ascension of ascending node: | 340.0111° |
| argument of perigee: | 89.4470° |
| revolutions per day: | 13.18687539 |
| mean anomaly at epoch: | 270.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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