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 54243U 26145.41721333 +.00000000 +00000-0 +00000-0 0 00003
2 54243 0.0265 110.9887 0001416 310.7626 210.4475 1.00272161 07
| Epoch (UTC): | 25 May 2026 10:00:47 |
| Eccentricity: | 0.0001416 |
| inclination: | 0.0265° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 110.9887° |
| argument of perigee: | 310.7626° |
| revolutions per day: | 1.00272161 |
| mean anomaly at epoch: | 210.4475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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