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 49740U 26145.32687913 +.00000000 +00000-0 +48733-4 0 00003
2 49740 53.2163 165.0533 0001482 79.8347 280.2813 15.08843803 06
| Epoch (UTC): | 25 May 2026 07:50:42 |
| Eccentricity: | 0.0001482 |
| inclination: | 53.2163° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 165.0533° |
| argument of perigee: | 79.8347° |
| revolutions per day: | 15.08843803 |
| mean anomaly at epoch: | 280.2813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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