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 42063U 26063.17252812 +.00000000 +00000-0 +68577-4 0 00000
2 42063 98.5672 139.4465 0001088 94.7740 265.3567 14.30817447 07
| Epoch (UTC): | 04 March 2026 04:08:26 |
| Eccentricity: | 0.0001088 |
| inclination: | 98.5672° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 139.4465° |
| argument of perigee: | 94.7740° |
| revolutions per day: | 14.30817447 |
| mean anomaly at epoch: | 265.3567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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