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 54181U 26145.34844683 +.00000000 +00000-0 +46301-3 0 00007
2 54181 53.2119 19.7599 0001305 95.4000 264.7140 15.08808727 09
| Epoch (UTC): | 25 May 2026 08:21:45 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.7599° |
| argument of perigee: | 95.4000° |
| revolutions per day: | 15.08808727 |
| mean anomaly at epoch: | 264.7140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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