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 63021U 26145.03265549 +.00000000 +00000-0 +57853-3 0 00008
2 63021 43.0012 265.0810 0001148 284.4969 75.5755 15.27574410 02
| Epoch (UTC): | 25 May 2026 00:47:01 |
| Eccentricity: | 0.0001148 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 265.0810° |
| argument of perigee: | 284.4969° |
| revolutions per day: | 15.27574410 |
| mean anomaly at epoch: | 75.5755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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