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 63448U 26145.36927942 +.00000000 +00000-0 +67256-3 0 00007
2 63448 53.1584 143.5407 0000586 118.4466 241.6599 15.42179003 04
| Epoch (UTC): | 25 May 2026 08:51:45 |
| Eccentricity: | 0.0000586 |
| inclination: | 53.1584° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.5407° |
| argument of perigee: | 118.4466° |
| revolutions per day: | 15.42179003 |
| mean anomaly at epoch: | 241.6599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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