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 63443U 26145.31156735 +.00000000 +00000-0 +71737-3 0 00000
2 63443 53.1596 143.8954 0001090 97.1607 262.9523 15.42177786 02
| Epoch (UTC): | 25 May 2026 07:28:39 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1596° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.8954° |
| argument of perigee: | 97.1607° |
| revolutions per day: | 15.42177786 |
| mean anomaly at epoch: | 262.9523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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