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 63517U 26145.38464856 +.00000000 +00000-0 +35694-3 0 00007
2 63517 53.1603 143.5369 0001282 85.4400 274.6747 15.30200896 08
| Epoch (UTC): | 25 May 2026 09:13:53 |
| Eccentricity: | 0.0001282 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.5369° |
| argument of perigee: | 85.4400° |
| revolutions per day: | 15.30200896 |
| mean anomaly at epoch: | 274.6747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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