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 63745U 26145.05799250 +.00000000 +00000-0 +35839-3 0 00004
2 63745 51.8682 14.2777 0004946 47.2485 312.8919 15.39450626 02
| Epoch (UTC): | 25 May 2026 01:23:30 |
| Eccentricity: | 0.0004946 |
| inclination: | 51.8682° |
| perigee height: | 444 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 14.2777° |
| argument of perigee: | 47.2485° |
| revolutions per day: | 15.39450626 |
| mean anomaly at epoch: | 312.8919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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