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 63182U 26145.51343958 +.00000000 +00000-0 +13699-3 0 00000
2 63182 97.9579 330.7588 0008944 265.3075 94.7112 14.74014040 04
| Epoch (UTC): | 25 May 2026 12:19:21 |
| Eccentricity: | 0.0008944 |
| inclination: | 97.9579° |
| perigee height: | 642 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 330.7588° |
| argument of perigee: | 265.3075° |
| revolutions per day: | 14.74014040 |
| mean anomaly at epoch: | 94.7112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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