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 63111U 26145.25288671 +.00000000 +00000-0 +29896-2 0 00008
2 63111 42.9994 135.6323 0001172 232.8516 127.2244 15.70743348 06
| Epoch (UTC): | 25 May 2026 06:04:09 |
| Eccentricity: | 0.0001172 |
| inclination: | 42.9994° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 135.6323° |
| argument of perigee: | 232.8516° |
| revolutions per day: | 15.70743348 |
| mean anomaly at epoch: | 127.2244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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