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 63754U 26145.42931897 +.00000000 +00000-0 +12432-2 0 00003
2 63754 43.0029 189.7707 0002428 261.1390 98.9202 15.70858841 09
| Epoch (UTC): | 25 May 2026 10:18:13 |
| Eccentricity: | 0.0002428 |
| inclination: | 43.0029° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 189.7707° |
| argument of perigee: | 261.1390° |
| revolutions per day: | 15.70858841 |
| mean anomaly at epoch: | 98.9202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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