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 63808U 26145.25947531 +.00000000 +00000-0 +39574-3 0 00003
2 63808 43.0036 100.2386 0001228 260.0236 100.0477 15.27585578 07
| Epoch (UTC): | 25 May 2026 06:13:38 |
| Eccentricity: | 0.0001228 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2386° |
| argument of perigee: | 260.0236° |
| revolutions per day: | 15.27585578 |
| mean anomaly at epoch: | 100.0477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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