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 63372U 26145.16160036 +.00000000 +00000-0 +96367-3 0 00009
2 63372 53.1596 54.7010 0001263 87.9263 272.1882 15.30204726 06
| Epoch (UTC): | 25 May 2026 03:52:42 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 54.7010° |
| argument of perigee: | 87.9263° |
| revolutions per day: | 15.30204726 |
| mean anomaly at epoch: | 272.1882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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