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 49026U 26145.20041013 +.00000000 +00000-0 +17667-3 0 00003
2 49026 34.9941 53.2063 0005405 304.1150 55.9045 15.02577641 06
| Epoch (UTC): | 25 May 2026 04:48:35 |
| Eccentricity: | 0.0005405 |
| inclination: | 34.9941° |
| perigee height: | 555 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 53.2063° |
| argument of perigee: | 304.1150° |
| revolutions per day: | 15.02577641 |
| mean anomaly at epoch: | 55.9045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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