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 49746U 26145.35169052 +.00000000 +00000-0 +57166-4 0 00001
2 49746 53.2108 164.9732 0001067 68.6818 291.4288 15.08835745 04
| Epoch (UTC): | 25 May 2026 08:26:26 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.9732° |
| argument of perigee: | 68.6818° |
| revolutions per day: | 15.08835745 |
| mean anomaly at epoch: | 291.4288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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