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 54009U 26145.23341998 +.00000000 +00000-0 -96926-5 0 00006
2 54009 53.2143 230.1066 0001183 94.6589 265.4538 15.08839925 03
| Epoch (UTC): | 25 May 2026 05:36:07 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 230.1066° |
| argument of perigee: | 94.6589° |
| revolutions per day: | 15.08839925 |
| mean anomaly at epoch: | 265.4538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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