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 50187U 26145.56604986 +.00000000 +00000-0 +94986-3 0 00005
2 50187 53.2145 253.4475 0000753 104.7749 255.3328 15.10993676 05
| Epoch (UTC): | 25 May 2026 13:35:06 |
| Eccentricity: | 0.0000753 |
| inclination: | 53.2145° |
| perigee height: | 533 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 253.4475° |
| argument of perigee: | 104.7749° |
| revolutions per day: | 15.10993676 |
| mean anomaly at epoch: | 255.3328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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