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 49741U 26145.32320062 +.00000000 +00000-0 +92588-4 0 00000
2 49741 53.2134 165.1072 0001097 73.0282 287.0830 15.08843132 09
| Epoch (UTC): | 25 May 2026 07:45:24 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 165.1072° |
| argument of perigee: | 73.0282° |
| revolutions per day: | 15.08843132 |
| mean anomaly at epoch: | 287.0830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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