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 63504U 26145.29412748 +.00000000 +00000-0 +48807-3 0 00006
2 63504 53.1566 144.4360 0000973 69.6621 290.4485 15.30206545 00
| Epoch (UTC): | 25 May 2026 07:03:32 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1566° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.4360° |
| argument of perigee: | 69.6621° |
| revolutions per day: | 15.30206545 |
| mean anomaly at epoch: | 290.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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