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 63973U 26145.25696448 +.00000000 +00000-0 +55234-3 0 00005
2 63973 43.0023 100.5657 0001580 275.1907 84.8765 15.27596242 02
| Epoch (UTC): | 25 May 2026 06:10:01 |
| Eccentricity: | 0.0001580 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.5657° |
| argument of perigee: | 275.1907° |
| revolutions per day: | 15.27596242 |
| mean anomaly at epoch: | 84.8765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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