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 49137U 26145.22877013 +.00000000 +00000-0 -97822-4 0 00008
2 49137 69.9998 82.5041 0003142 267.3209 92.7590 14.97520729 03
| Epoch (UTC): | 25 May 2026 05:29:25 |
| Eccentricity: | 0.0003142 |
| inclination: | 69.9998° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 82.5041° |
| argument of perigee: | 267.3209° |
| revolutions per day: | 14.97520729 |
| mean anomaly at epoch: | 92.7590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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