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 57737U 26145.36296935 +.00000000 +00000-0 +11050-3 0 00003
2 57737 43.0023 112.9907 0000127 53.5272 306.5583 15.06013641 03
| Epoch (UTC): | 25 May 2026 08:42:40 |
| Eccentricity: | 0.0000127 |
| inclination: | 43.0023° |
| perigee height: | 548 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 112.9907° |
| argument of perigee: | 53.5272° |
| revolutions per day: | 15.06013641 |
| mean anomaly at epoch: | 306.5583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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