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 63720U 26145.59303495 +.00000000 +00000-0 +19548-4 0 00008
2 63720 53.1589 222.3570 0001083 91.8757 268.2368 15.30163995 08
| Epoch (UTC): | 25 May 2026 14:13:58 |
| Eccentricity: | 0.0001083 |
| inclination: | 53.1589° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.3570° |
| argument of perigee: | 91.8757° |
| revolutions per day: | 15.30163995 |
| mean anomaly at epoch: | 268.2368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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