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 57165U 26086.93042247 +.00000000 +00000-0 +63605-4 0 00004
2 57165 74.0493 154.6745 0022600 283.5328 76.3307 14.36353206 05
| Epoch (UTC): | 27 March 2026 22:19:48 |
| Eccentricity: | 0.0022600 |
| inclination: | 74.0493° |
| perigee height: | 754 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 154.6745° |
| argument of perigee: | 283.5328° |
| revolutions per day: | 14.36353206 |
| mean anomaly at epoch: | 76.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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