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 63314U 26145.41791469 +.00000000 +00000-0 +99516-3 0 00002
2 63314 42.9984 162.1566 0000426 257.6793 102.4027 15.70857179 09
| Epoch (UTC): | 25 May 2026 10:01:47 |
| Eccentricity: | 0.0000426 |
| inclination: | 42.9984° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.1566° |
| argument of perigee: | 257.6793° |
| revolutions per day: | 15.70857179 |
| mean anomaly at epoch: | 102.4027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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