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 57139U 26145.43139186 +.00000000 +00000-0 +79228-4 0 00003
2 57139 43.0030 189.6394 0001293 272.7741 87.2963 15.27576267 05
| Epoch (UTC): | 25 May 2026 10:21:12 |
| Eccentricity: | 0.0001293 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.6394° |
| argument of perigee: | 272.7741° |
| revolutions per day: | 15.27576267 |
| mean anomaly at epoch: | 87.2963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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