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 63507U 26145.26351838 +.00000000 +00000-0 +28976-3 0 00003
2 63507 53.1588 144.2113 0001403 95.1330 264.9831 15.30202532 04
| Epoch (UTC): | 25 May 2026 06:19:27 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.2113° |
| argument of perigee: | 95.1330° |
| revolutions per day: | 15.30202532 |
| mean anomaly at epoch: | 264.9831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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