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 63714U 26145.37596735 +.00000000 +00000-0 +34208-3 0 00007
2 63714 53.1574 223.1383 0001224 65.9002 294.2126 15.30203906 06
| Epoch (UTC): | 25 May 2026 09:01:23 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.1383° |
| argument of perigee: | 65.9002° |
| revolutions per day: | 15.30203906 |
| mean anomaly at epoch: | 294.2126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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