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 63137U 26145.29383534 +.00000000 +00000-0 +13376-2 0 00000
2 63137 43.0028 148.6405 0004161 278.7647 81.2750 15.70850686 09
| Epoch (UTC): | 25 May 2026 07:03:07 |
| Eccentricity: | 0.0004161 |
| inclination: | 43.0028° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 148.6405° |
| argument of perigee: | 278.7647° |
| revolutions per day: | 15.70850686 |
| mean anomaly at epoch: | 81.2750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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