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 63192U 26145.57848853 +.00000000 +00000-0 +11714-2 0 00006
2 63192 42.9987 216.4465 0000729 26.7965 333.2941 15.70831790 09
| Epoch (UTC): | 25 May 2026 13:53:01 |
| Eccentricity: | 0.0000729 |
| inclination: | 42.9987° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 216.4465° |
| argument of perigee: | 26.7965° |
| revolutions per day: | 15.70831790 |
| mean anomaly at epoch: | 333.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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