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 55368U 26145.17821567 +.00000000 +00000-0 +72199-5 0 00008
2 55368 43.0049 216.5304 0001959 276.9267 83.1361 15.27576379 07
| Epoch (UTC): | 25 May 2026 04:16:37 |
| Eccentricity: | 0.0001959 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 216.5304° |
| argument of perigee: | 276.9267° |
| revolutions per day: | 15.27576379 |
| mean anomaly at epoch: | 83.1361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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