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 59112U 26107.19212755 +.00000000 +00000-0 +36740-3 0 00002
2 59112 97.5463 254.0841 0007217 71.2195 288.9841 15.54416878 09
| Epoch (UTC): | 17 April 2026 04:36:39 |
| Eccentricity: | 0.0007217 |
| inclination: | 97.5463° |
| perigee height: | 399 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 254.0841° |
| argument of perigee: | 71.2195° |
| revolutions per day: | 15.54416878 |
| mean anomaly at epoch: | 288.9841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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