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 57413U 26145.29603259 +.00000000 +00000-0 +17873-4 0 00007
2 57413 43.0033 114.0159 0001136 281.3100 78.7624 15.27577429 05
| Epoch (UTC): | 25 May 2026 07:06:17 |
| Eccentricity: | 0.0001136 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.0159° |
| argument of perigee: | 281.3100° |
| revolutions per day: | 15.27577429 |
| mean anomaly at epoch: | 78.7624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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