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 63963U 26145.36027189 +.00000000 +00000-0 +71315-3 0 00004
2 63963 43.0009 103.0839 0001516 261.1463 98.9217 15.27597948 08
| Epoch (UTC): | 25 May 2026 08:38:47 |
| Eccentricity: | 0.0001516 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.0839° |
| argument of perigee: | 261.1463° |
| revolutions per day: | 15.27597948 |
| mean anomaly at epoch: | 98.9217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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