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 46054U 26145.20917941 +.00000000 +00000-0 +16428-3 0 00007
2 46054 53.1581 118.1961 0001097 88.9430 271.1697 15.31719040 04
| Epoch (UTC): | 25 May 2026 05:01:13 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 118.1961° |
| argument of perigee: | 88.9430° |
| revolutions per day: | 15.31719040 |
| mean anomaly at epoch: | 271.1697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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