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 63051U 26145.35526049 +.00000000 +00000-0 +77846-3 0 00005
2 63051 53.1590 274.1699 0001758 103.0509 257.0690 15.34400804 05
| Epoch (UTC): | 25 May 2026 08:31:34 |
| Eccentricity: | 0.0001758 |
| inclination: | 53.1590° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 274.1699° |
| argument of perigee: | 103.0509° |
| revolutions per day: | 15.34400804 |
| mean anomaly at epoch: | 257.0690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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