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 57775U 26145.38758556 +.00000000 +00000-0 +11815-4 0 00009
2 57775 43.0036 121.6092 0001430 302.4657 57.6056 15.27572379 02
| Epoch (UTC): | 25 May 2026 09:18:07 |
| Eccentricity: | 0.0001430 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.6092° |
| argument of perigee: | 302.4657° |
| revolutions per day: | 15.27572379 |
| mean anomaly at epoch: | 57.6056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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