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 57244U 26145.17842390 +.00000000 +00000-0 -32105-4 0 00003
2 57244 43.0054 307.4367 0002050 261.0639 98.9980 15.27575757 08
| Epoch (UTC): | 25 May 2026 04:16:55 |
| Eccentricity: | 0.0002050 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 307.4367° |
| argument of perigee: | 261.0639° |
| revolutions per day: | 15.27575757 |
| mean anomaly at epoch: | 98.9980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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