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 04071U 26064.66064456 +.00000000 +00000-0 +16943-3 0 00006
2 04071 74.0484 136.2047 0013509 8.0515 352.0868 14.66572931 07
| Epoch (UTC): | 05 March 2026 15:51:19 |
| Eccentricity: | 0.0013509 |
| inclination: | 74.0484° |
| perigee height: | 663 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 136.2047° |
| argument of perigee: | 8.0515° |
| revolutions per day: | 14.66572931 |
| mean anomaly at epoch: | 352.0868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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