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 59846U 26145.47492595 +.00000000 +00000-0 +81862-5 0 00008
2 59846 43.0024 200.4115 0001350 277.4933 82.5766 15.27580683 03
| Epoch (UTC): | 25 May 2026 11:23:53 |
| Eccentricity: | 0.0001350 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.4115° |
| argument of perigee: | 277.4933° |
| revolutions per day: | 15.27580683 |
| mean anomaly at epoch: | 82.5766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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