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 57826U 26145.49277779 +.00000000 +00000-0 +19580-3 0 00007
2 57826 43.0037 160.4945 0001394 292.4924 67.5780 15.27573849 09
| Epoch (UTC): | 25 May 2026 11:49:36 |
| Eccentricity: | 0.0001394 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.4945° |
| argument of perigee: | 292.4924° |
| revolutions per day: | 15.27573849 |
| mean anomaly at epoch: | 67.5780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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