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 49457U 26145.23214774 +.00000000 +00000-0 +12930-3 0 00008
2 49457 53.2127 235.5169 0001369 88.1251 271.9898 15.08827580 04
| Epoch (UTC): | 25 May 2026 05:34:17 |
| Eccentricity: | 0.0001369 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 235.5169° |
| argument of perigee: | 88.1251° |
| revolutions per day: | 15.08827580 |
| mean anomaly at epoch: | 271.9898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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