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 57409U 26145.53577278 +.00000000 +00000-0 +57642-4 0 00008
2 57409 43.0040 174.5038 0001632 283.1425 76.9245 15.27576176 03
| Epoch (UTC): | 25 May 2026 12:51:30 |
| Eccentricity: | 0.0001632 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.5038° |
| argument of perigee: | 283.1425° |
| revolutions per day: | 15.27576176 |
| mean anomaly at epoch: | 76.9245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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