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 63153U 26145.15064163 +.00000000 +00000-0 +45704-3 0 00008
2 63153 97.4546 219.2575 0010441 137.0119 223.1929 15.11550698 07
| Epoch (UTC): | 25 May 2026 03:36:55 |
| Eccentricity: | 0.0010441 |
| inclination: | 97.4546° |
| perigee height: | 524 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 219.2575° |
| argument of perigee: | 137.0119° |
| revolutions per day: | 15.11550698 |
| mean anomaly at epoch: | 223.1929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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