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 63912U 26145.23596530 +.00000000 +00000-0 +49728-3 0 00008
2 63912 42.9990 103.9999 0001382 259.1120 100.9576 15.27563779 00
| Epoch (UTC): | 25 May 2026 05:39:47 |
| Eccentricity: | 0.0001382 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.9999° |
| argument of perigee: | 259.1120° |
| revolutions per day: | 15.27563779 |
| mean anomaly at epoch: | 100.9576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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