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 63549U 26145.46232931 +.00000000 +00000-0 +17280-2 0 00008
2 63549 42.9991 50.9801 0001179 97.0258 263.0744 15.70880865 09
| Epoch (UTC): | 25 May 2026 11:05:45 |
| Eccentricity: | 0.0001179 |
| inclination: | 42.9991° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 50.9801° |
| argument of perigee: | 97.0258° |
| revolutions per day: | 15.70880865 |
| mean anomaly at epoch: | 263.0744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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