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 50140U 26087.69344244 +.00000000 +00000-0 +37022-3 0 00009
2 50140 45.0156 86.9741 0004703 249.7602 110.2744 14.45648393 08
| Epoch (UTC): | 28 March 2026 16:38:33 |
| Eccentricity: | 0.0004703 |
| inclination: | 45.0156° |
| perigee height: | 737 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 86.9741° |
| argument of perigee: | 249.7602° |
| revolutions per day: | 14.45648393 |
| mean anomaly at epoch: | 110.2744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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