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 63976U 26145.24540049 +.00000000 +00000-0 +62375-3 0 00006
2 63976 43.0014 100.4758 0001245 271.1523 88.9186 15.27596838 07
| Epoch (UTC): | 25 May 2026 05:53:22 |
| Eccentricity: | 0.0001245 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.4758° |
| argument of perigee: | 271.1523° |
| revolutions per day: | 15.27596838 |
| mean anomaly at epoch: | 88.9186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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