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 63319U 26145.40197618 +.00000000 +00000-0 +12759-2 0 00005
2 63319 43.0030 162.0299 0003667 258.5280 101.5176 15.70973370 08
| Epoch (UTC): | 25 May 2026 09:38:50 |
| Eccentricity: | 0.0003667 |
| inclination: | 43.0030° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 162.0299° |
| argument of perigee: | 258.5280° |
| revolutions per day: | 15.70973370 |
| mean anomaly at epoch: | 101.5176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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