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 63576U 26145.32932411 +.00000000 +00000-0 +65190-3 0 00007
2 63576 43.0000 248.6876 0000450 281.2275 78.8526 15.27575965 01
| Epoch (UTC): | 25 May 2026 07:54:13 |
| Eccentricity: | 0.0000450 |
| inclination: | 43.0000° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 248.6876° |
| argument of perigee: | 281.2275° |
| revolutions per day: | 15.27575965 |
| mean anomaly at epoch: | 78.8526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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