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 57869U 26145.21715016 +.00000000 +00000-0 +33780-4 0 00004
2 57869 43.0015 212.7754 0001438 281.6203 78.4487 15.27572722 04
| Epoch (UTC): | 25 May 2026 05:12:41 |
| Eccentricity: | 0.0001438 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.7754° |
| argument of perigee: | 281.6203° |
| revolutions per day: | 15.27572722 |
| mean anomaly at epoch: | 78.4487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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