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 54086U 26145.26613925 +.00000000 +00000-0 +25655-4 0 00005
2 54086 53.2142 335.4558 0001144 104.2188 255.8932 15.08836134 02
| Epoch (UTC): | 25 May 2026 06:23:14 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 335.4558° |
| argument of perigee: | 104.2188° |
| revolutions per day: | 15.08836134 |
| mean anomaly at epoch: | 255.8932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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