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 49433U 26145.20632977 +.00000000 +00000-0 +41902-4 0 00000
2 49433 53.2141 225.6251 0001133 85.7447 274.3674 15.08836320 06
| Epoch (UTC): | 25 May 2026 04:57:06 |
| Eccentricity: | 0.0001133 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 225.6251° |
| argument of perigee: | 85.7447° |
| revolutions per day: | 15.08836320 |
| mean anomaly at epoch: | 274.3674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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