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 63749U 26145.58335647 +.00000000 +00000-0 -41384-2 0 00004
2 63749 51.8986 131.9500 0000675 101.7459 235.7810 14.82214462 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000675 |
| inclination: | 51.8986° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 131.9500° |
| argument of perigee: | 101.7459° |
| revolutions per day: | 14.82214462 |
| mean anomaly at epoch: | 235.7810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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