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 57132U 26145.58173411 +.00000000 +00000-0 +67907-5 0 00003
2 57132 43.0017 207.1615 0001106 267.6846 92.3879 15.27572653 05
| Epoch (UTC): | 25 May 2026 13:57:41 |
| Eccentricity: | 0.0001106 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.1615° |
| argument of perigee: | 267.6846° |
| revolutions per day: | 15.27572653 |
| mean anomaly at epoch: | 92.3879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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