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 49432U 26145.53756443 +.00000000 +00000-0 -52475-4 0 00008
2 49432 53.2120 234.1351 0001329 85.9313 274.1831 15.08841279 01
| Epoch (UTC): | 25 May 2026 12:54:05 |
| Eccentricity: | 0.0001329 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.1351° |
| argument of perigee: | 85.9313° |
| revolutions per day: | 15.08841279 |
| mean anomaly at epoch: | 274.1831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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