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 55384U 26145.59521683 +.00000000 +00000-0 +44971-4 0 00004
2 55384 43.0033 243.9015 0001844 288.3632 71.7019 15.27581270 06
| Epoch (UTC): | 25 May 2026 14:17:06 |
| Eccentricity: | 0.0001844 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.9015° |
| argument of perigee: | 288.3632° |
| revolutions per day: | 15.27581270 |
| mean anomaly at epoch: | 71.7019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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