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 63977U 26145.17744701 +.00000000 +00000-0 +59506-3 0 00002
2 63977 43.0022 100.8252 0000817 277.7046 82.3713 15.27591186 01
| Epoch (UTC): | 25 May 2026 04:15:31 |
| Eccentricity: | 0.0000817 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.8252° |
| argument of perigee: | 277.7046° |
| revolutions per day: | 15.27591186 |
| mean anomaly at epoch: | 82.3713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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