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 63018U 26145.02494837 +.00000000 +00000-0 +10069-2 0 00004
2 63018 42.9992 265.0174 0001423 33.4659 326.6283 15.27586513 03
| Epoch (UTC): | 25 May 2026 00:35:55 |
| Eccentricity: | 0.0001423 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 265.0174° |
| argument of perigee: | 33.4659° |
| revolutions per day: | 15.27586513 |
| mean anomaly at epoch: | 326.6283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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