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 63437U 26145.26137289 +.00000000 +00000-0 +73490-3 0 00008
2 63437 53.1584 144.2943 0001420 90.5504 269.5665 15.42181903 01
| Epoch (UTC): | 25 May 2026 06:16:22 |
| Eccentricity: | 0.0001420 |
| inclination: | 53.1584° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 144.2943° |
| argument of perigee: | 90.5504° |
| revolutions per day: | 15.42181903 |
| mean anomaly at epoch: | 269.5665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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