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 49431U 26145.55042873 +.00000000 +00000-0 +28611-4 0 00008
2 49431 53.2163 244.2603 0001442 88.9697 271.1461 15.08838164 08
| Epoch (UTC): | 25 May 2026 13:12:37 |
| Eccentricity: | 0.0001442 |
| inclination: | 53.2163° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 244.2603° |
| argument of perigee: | 88.9697° |
| revolutions per day: | 15.08838164 |
| mean anomaly at epoch: | 271.1461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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