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 63347U 26145.58021343 +.00000000 +00000-0 +20667-3 0 00004
2 63347 97.6118 327.1010 0011046 217.9139 142.1314 15.10840897 04
| Epoch (UTC): | 25 May 2026 13:55:30 |
| Eccentricity: | 0.0011046 |
| inclination: | 97.6118° |
| perigee height: | 526 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 327.1010° |
| argument of perigee: | 217.9139° |
| revolutions per day: | 15.10840897 |
| mean anomaly at epoch: | 142.1314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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