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 63560U 26145.13909095 +.00000000 +00000-0 +15495-2 0 00003
2 63560 43.0007 52.8499 0001678 256.7071 103.3609 15.70905588 03
| Epoch (UTC): | 25 May 2026 03:20:17 |
| Eccentricity: | 0.0001678 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 52.8499° |
| argument of perigee: | 256.7071° |
| revolutions per day: | 15.70905588 |
| mean anomaly at epoch: | 103.3609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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