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 63676U 26145.48978946 +.00000000 +00000-0 +12629-2 0 00006
2 63676 43.0031 175.2057 0004145 261.2302 98.8096 15.70934030 00
| Epoch (UTC): | 25 May 2026 11:45:17 |
| Eccentricity: | 0.0004145 |
| inclination: | 43.0031° |
| perigee height: | 353 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 175.2057° |
| argument of perigee: | 261.2302° |
| revolutions per day: | 15.70934030 |
| mean anomaly at epoch: | 98.8096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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