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 54168U 26145.37792075 +.00000000 +00000-0 +64396-4 0 00007
2 54168 53.2145 19.9435 0001185 83.6025 276.5102 15.08835140 04
| Epoch (UTC): | 25 May 2026 09:04:12 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.9435° |
| argument of perigee: | 83.6025° |
| revolutions per day: | 15.08835140 |
| mean anomaly at epoch: | 276.5102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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