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 54021U 26088.23278603 +.00000000 +00000-0 +24041-3 0 00004
2 54021 54.9989 174.3763 0012117 244.4015 115.5726 14.62171839 00
| Epoch (UTC): | 29 March 2026 05:35:12 |
| Eccentricity: | 0.0012117 |
| inclination: | 54.9989° |
| perigee height: | 678 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 174.3763° |
| argument of perigee: | 244.4015° |
| revolutions per day: | 14.62171839 |
| mean anomaly at epoch: | 115.5726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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