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 54192U 26145.34199456 +.00000000 +00000-0 +59065-4 0 00002
2 54192 53.2146 9.7381 0001353 81.5547 278.5599 15.08839933 08
| Epoch (UTC): | 25 May 2026 08:12:28 |
| Eccentricity: | 0.0001353 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 9.7381° |
| argument of perigee: | 81.5547° |
| revolutions per day: | 15.08839933 |
| mean anomaly at epoch: | 278.5599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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