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 57995U 26144.99699163 +.00000000 +00000-0 +39755-4 0 00000
2 57995 43.0023 356.3617 0001263 262.8353 97.2355 15.27567257 09
| Epoch (UTC): | 24 May 2026 23:55:40 |
| Eccentricity: | 0.0001263 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.3617° |
| argument of perigee: | 262.8353° |
| revolutions per day: | 15.27567257 |
| mean anomaly at epoch: | 97.2355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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