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 63113U 26145.36410201 +.00000000 +00000-0 +19077-2 0 00008
2 63113 43.0000 134.7390 0001423 263.0705 97.0001 15.70921012 08
| Epoch (UTC): | 25 May 2026 08:44:18 |
| Eccentricity: | 0.0001423 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 134.7390° |
| argument of perigee: | 263.0705° |
| revolutions per day: | 15.70921012 |
| mean anomaly at epoch: | 97.0001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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