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 49411U 26145.61758042 +.00000000 +00000-0 -69201-4 0 00006
2 49411 53.2141 233.7772 0001060 71.4718 288.6389 15.08825245 07
| Epoch (UTC): | 25 May 2026 14:49:18 |
| Eccentricity: | 0.0001060 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 233.7772° |
| argument of perigee: | 71.4718° |
| revolutions per day: | 15.08825245 |
| mean anomaly at epoch: | 288.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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