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 57359U 26145.55601352 +.00000000 +00000-0 -14320-4 0 00002
2 57359 43.0006 167.6984 0001243 268.1280 91.9430 15.27570590 09
| Epoch (UTC): | 25 May 2026 13:20:39 |
| Eccentricity: | 0.0001243 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.6984° |
| argument of perigee: | 268.1280° |
| revolutions per day: | 15.27570590 |
| mean anomaly at epoch: | 91.9430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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