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 63721U 26145.51442539 +.00000000 +00000-0 +45976-3 0 00007
2 63721 53.1583 222.5848 0001153 95.2800 264.8333 15.31720245 00
| Epoch (UTC): | 25 May 2026 12:20:46 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.5848° |
| argument of perigee: | 95.2800° |
| revolutions per day: | 15.31720245 |
| mean anomaly at epoch: | 264.8333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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