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 54818U 26145.59052693 +.00000000 +00000-0 +23257-3 0 00008
2 54818 97.4195 279.0443 0007623 50.0033 310.1872 15.23565853 06
| Epoch (UTC): | 25 May 2026 14:10:21 |
| Eccentricity: | 0.0007623 |
| inclination: | 97.4195° |
| perigee height: | 490 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 279.0443° |
| argument of perigee: | 50.0033° |
| revolutions per day: | 15.23565853 |
| mean anomaly at epoch: | 310.1872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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