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 57800U 26145.42085699 +.00000000 +00000-0 +22865-3 0 00000
2 57800 31.0009 147.0486 0007537 94.5976 265.5524 15.12232447 07
| Epoch (UTC): | 25 May 2026 10:06:02 |
| Eccentricity: | 0.0007537 |
| inclination: | 31.0009° |
| perigee height: | 524 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 147.0486° |
| argument of perigee: | 94.5976° |
| revolutions per day: | 15.12232447 |
| mean anomaly at epoch: | 265.5524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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