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 57841U 26145.13461086 +.00000000 +00000-0 +56260-4 0 00008
2 57841 53.1610 288.7391 0001219 83.7432 276.3709 15.31705107 05
| Epoch (UTC): | 25 May 2026 03:13:50 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 288.7391° |
| argument of perigee: | 83.7432° |
| revolutions per day: | 15.31705107 |
| mean anomaly at epoch: | 276.3709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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