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 54092U 26145.40913632 +.00000000 +00000-0 +48364-3 0 00007
2 54092 53.1724 154.3659 0003739 32.5127 327.6125 15.78482860 04
| Epoch (UTC): | 25 May 2026 09:49:09 |
| Eccentricity: | 0.0003739 |
| inclination: | 53.1724° |
| perigee height: | 332 km |
| apogee height: | 337 km |
| right ascension of ascending node: | 154.3659° |
| argument of perigee: | 32.5127° |
| revolutions per day: | 15.78482860 |
| mean anomaly at epoch: | 327.6125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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