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 50181U 26145.04536707 +.00000000 +00000-0 +67531-4 0 00004
2 50181 53.2145 266.3548 0001284 89.6582 270.4557 15.08838365 01
| Epoch (UTC): | 25 May 2026 01:05:19 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 266.3548° |
| argument of perigee: | 89.6582° |
| revolutions per day: | 15.08838365 |
| mean anomaly at epoch: | 270.4557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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