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 57141U 26145.43268654 +.00000000 +00000-0 +52150-4 0 00004
2 57141 43.0000 189.6504 0001362 298.8516 61.2198 15.27583575 06
| Epoch (UTC): | 25 May 2026 10:23:04 |
| Eccentricity: | 0.0001362 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.6504° |
| argument of perigee: | 298.8516° |
| revolutions per day: | 15.27583575 |
| mean anomaly at epoch: | 61.2198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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