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 57343U 26145.66668980 +.00000000 +00000-0 +40711-3 0 00008
2 57343 42.9999 177.9767 0001046 272.8251 153.5048 15.27576916 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001046 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 177.9767° |
| argument of perigee: | 272.8251° |
| revolutions per day: | 15.27576916 |
| mean anomaly at epoch: | 153.5048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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