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 49767U 26145.41884683 +.00000000 +00000-0 +13855-4 0 00002
2 49767 53.2118 154.6702 0000807 66.0429 294.0647 15.08841365 05
| Epoch (UTC): | 25 May 2026 10:03:08 |
| Eccentricity: | 0.0000807 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 154.6702° |
| argument of perigee: | 66.0429° |
| revolutions per day: | 15.08841365 |
| mean anomaly at epoch: | 294.0647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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