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 57416U 26145.54604846 +.00000000 +00000-0 +30750-4 0 00000
2 57416 43.0021 174.5716 0001400 261.5172 98.5521 15.27580548 00
| Epoch (UTC): | 25 May 2026 13:06:18 |
| Eccentricity: | 0.0001400 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.5716° |
| argument of perigee: | 261.5172° |
| revolutions per day: | 15.27580548 |
| mean anomaly at epoch: | 98.5521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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