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 57410U 26145.53079118 +.00000000 +00000-0 +86507-4 0 00002
2 57410 43.0028 175.3116 0001279 271.8876 88.1829 15.27559283 01
| Epoch (UTC): | 25 May 2026 12:44:20 |
| Eccentricity: | 0.0001279 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.3116° |
| argument of perigee: | 271.8876° |
| revolutions per day: | 15.27559283 |
| mean anomaly at epoch: | 88.1829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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