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 57732U 26145.53683731 +.00000000 +00000-0 +13700-3 0 00005
2 57732 43.0093 83.6104 0001411 264.7857 95.2834 15.27585736 03
| Epoch (UTC): | 25 May 2026 12:53:02 |
| Eccentricity: | 0.0001411 |
| inclination: | 43.0093° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.6104° |
| argument of perigee: | 264.7857° |
| revolutions per day: | 15.27585736 |
| mean anomaly at epoch: | 95.2834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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