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 57302U 26145.37102970 +.00000000 +00000-0 +25555-4 0 00003
2 57302 43.0014 150.1973 0001412 272.4192 87.6498 15.27576950 01
| Epoch (UTC): | 25 May 2026 08:54:16 |
| Eccentricity: | 0.0001412 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1973° |
| argument of perigee: | 272.4192° |
| revolutions per day: | 15.27576950 |
| mean anomaly at epoch: | 87.6498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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