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 54020U 26088.20995728 +.00000000 +00000-0 +29146-3 0 00005
2 54020 54.9986 172.9651 0010329 242.6296 117.3647 14.62857923 07
| Epoch (UTC): | 29 March 2026 05:02:20 |
| Eccentricity: | 0.0010329 |
| inclination: | 54.9986° |
| perigee height: | 677 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 172.9651° |
| argument of perigee: | 242.6296° |
| revolutions per day: | 14.62857923 |
| mean anomaly at epoch: | 117.3647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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