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 63770U 26145.21373450 +.00000000 +00000-0 +96771-3 0 00002
2 63770 43.0029 332.8288 0001078 281.9669 78.1062 15.27585080 09
| Epoch (UTC): | 25 May 2026 05:07:46 |
| Eccentricity: | 0.0001078 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 332.8288° |
| argument of perigee: | 281.9669° |
| revolutions per day: | 15.27585080 |
| mean anomaly at epoch: | 78.1062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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