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 63356U 26145.35667088 +.00000000 +00000-0 +21458-3 0 00000
2 63356 97.5595 121.4724 0017192 332.0336 27.9970 15.14587879 05
| Epoch (UTC): | 25 May 2026 08:33:36 |
| Eccentricity: | 0.0017192 |
| inclination: | 97.5595° |
| perigee height: | 510 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 121.4724° |
| argument of perigee: | 332.0336° |
| revolutions per day: | 15.14587879 |
| mean anomaly at epoch: | 27.9970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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