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 57788U 26145.27983272 +.00000000 +00000-0 +13736-4 0 00000
2 57788 43.0032 110.5467 0001533 284.4727 75.5954 15.27579466 06
| Epoch (UTC): | 25 May 2026 06:42:57 |
| Eccentricity: | 0.0001533 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.5467° |
| argument of perigee: | 284.4727° |
| revolutions per day: | 15.27579466 |
| mean anomaly at epoch: | 75.5954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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