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 49749U 26145.43731779 +.00000000 +00000-0 +28250-4 0 00006
2 49749 53.2116 164.8284 0001349 91.0377 269.0770 15.08837142 00
| Epoch (UTC): | 25 May 2026 10:29:44 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.8284° |
| argument of perigee: | 91.0377° |
| revolutions per day: | 15.08837142 |
| mean anomaly at epoch: | 269.0770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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