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 57909U 26145.54313282 +.00000000 +00000-0 +86344-4 0 00008
2 57909 42.9974 240.7101 0001411 270.5485 89.5205 15.27581740 09
| Epoch (UTC): | 25 May 2026 13:02:06 |
| Eccentricity: | 0.0001411 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.7101° |
| argument of perigee: | 270.5485° |
| revolutions per day: | 15.27581740 |
| mean anomaly at epoch: | 89.5205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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