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 56171U 26088.17871963 +.00000000 +00000-0 +16581-3 0 00003
2 56171 81.0037 157.0716 0017258 155.0207 205.1787 13.82412259 08
| Epoch (UTC): | 29 March 2026 04:17:21 |
| Eccentricity: | 0.0017258 |
| inclination: | 81.0037° |
| perigee height: | 943 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 157.0716° |
| argument of perigee: | 155.0207° |
| revolutions per day: | 13.82412259 |
| mean anomaly at epoch: | 205.1787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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