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 63318U 26145.32777959 +.00000000 +00000-0 +12995-2 0 00009
2 63318 43.0010 162.3230 0001917 270.5461 89.5187 15.70854206 07
| Epoch (UTC): | 25 May 2026 07:52:00 |
| Eccentricity: | 0.0001917 |
| inclination: | 43.0010° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 162.3230° |
| argument of perigee: | 270.5461° |
| revolutions per day: | 15.70854206 |
| mean anomaly at epoch: | 89.5187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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