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 63515U 26145.31194925 +.00000000 +00000-0 +37610-3 0 00005
2 63515 53.1599 143.7975 0001203 86.4695 273.6443 15.30199095 05
| Epoch (UTC): | 25 May 2026 07:29:12 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.7975° |
| argument of perigee: | 86.4695° |
| revolutions per day: | 15.30199095 |
| mean anomaly at epoch: | 273.6443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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