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 63104U 26145.02494936 +.00000000 +00000-0 +10075-2 0 00007
2 63104 42.9976 136.4864 0001511 200.2819 159.7988 15.70875301 09
| Epoch (UTC): | 25 May 2026 00:35:55 |
| Eccentricity: | 0.0001511 |
| inclination: | 42.9976° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 136.4864° |
| argument of perigee: | 200.2819° |
| revolutions per day: | 15.70875301 |
| mean anomaly at epoch: | 159.7988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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