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 63767U 26145.55865894 +.00000000 +00000-0 +65680-3 0 00008
2 63767 43.0033 331.1227 0001298 267.7948 92.2755 15.27588636 07
| Epoch (UTC): | 25 May 2026 13:24:28 |
| Eccentricity: | 0.0001298 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.1227° |
| argument of perigee: | 267.7948° |
| revolutions per day: | 15.27588636 |
| mean anomaly at epoch: | 92.2755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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