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 59588U 26161.52963198 +.00000000 +00000-0 +50390-2 0 00006
2 59588 97.1673 81.8047 0057401 68.3969 292.3300 13.93911964 01
| Epoch (UTC): | 10 June 2026 12:42:40 |
| Eccentricity: | 0.0057401 |
| inclination: | 97.1673° |
| perigee height: | 873 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 81.8047° |
| argument of perigee: | 68.3969° |
| revolutions per day: | 13.93911964 |
| mean anomaly at epoch: | 292.3300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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