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 63716U 26145.58901014 +.00000000 +00000-0 +41382-3 0 00003
2 63716 53.1587 222.3347 0000495 29.3693 330.7336 15.31717931 00
| Epoch (UTC): | 25 May 2026 14:08:10 |
| Eccentricity: | 0.0000495 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.3347° |
| argument of perigee: | 29.3693° |
| revolutions per day: | 15.31717931 |
| mean anomaly at epoch: | 330.7336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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