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 63430U 26145.42606675 +.00000000 +00000-0 +20541-3 0 00008
2 63430 54.9907 127.6704 0004522 275.8378 84.2128 15.25085215 01
| Epoch (UTC): | 25 May 2026 10:13:32 |
| Eccentricity: | 0.0004522 |
| inclination: | 54.9907° |
| perigee height: | 487 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 127.6704° |
| argument of perigee: | 275.8378° |
| revolutions per day: | 15.25085215 |
| mean anomaly at epoch: | 84.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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