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 49443U 26145.48593043 +.00000000 +00000-0 +90657-3 0 00001
2 49443 53.2147 224.1737 0001824 24.2661 335.8417 15.10084892 09
| Epoch (UTC): | 25 May 2026 11:39:44 |
| Eccentricity: | 0.0001824 |
| inclination: | 53.2147° |
| perigee height: | 535 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 224.1737° |
| argument of perigee: | 24.2661° |
| revolutions per day: | 15.10084892 |
| mean anomaly at epoch: | 335.8417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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