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 63078U 26145.42186179 +.00000000 +00000-0 +16088-3 0 00009
2 63078 70.0006 161.0705 0004002 265.9461 94.1241 14.98335605 03
| Epoch (UTC): | 25 May 2026 10:07:28 |
| Eccentricity: | 0.0004002 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 161.0705° |
| argument of perigee: | 265.9461° |
| revolutions per day: | 14.98335605 |
| mean anomaly at epoch: | 94.1241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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