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 57408U 26145.43584233 +.00000000 +00000-0 -53434-5 0 00002
2 57408 43.0017 175.4692 0001429 271.5935 88.4753 15.27577636 07
| Epoch (UTC): | 25 May 2026 10:27:36 |
| Eccentricity: | 0.0001429 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.4692° |
| argument of perigee: | 271.5935° |
| revolutions per day: | 15.27577636 |
| mean anomaly at epoch: | 88.4753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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