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 53994U 26145.52417272 +.00000000 +00000-0 +52467-4 0 00009
2 53994 53.2121 229.0756 0001169 81.9119 278.2006 15.08833239 00
| Epoch (UTC): | 25 May 2026 12:34:48 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 229.0756° |
| argument of perigee: | 81.9119° |
| revolutions per day: | 15.08833239 |
| mean anomaly at epoch: | 278.2006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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