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 63498U 26145.27409397 +.00000000 +00000-0 +61661-3 0 00005
2 63498 53.1577 144.3137 0000958 91.2188 268.8923 15.30199274 03
| Epoch (UTC): | 25 May 2026 06:34:41 |
| Eccentricity: | 0.0000958 |
| inclination: | 53.1577° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.3137° |
| argument of perigee: | 91.2188° |
| revolutions per day: | 15.30199274 |
| mean anomaly at epoch: | 268.8923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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