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 39089U 26150.43942284 +.00000000 +00000-0 +82762-4 0 00001
2 39089 98.4172 330.8947 0009974 303.0977 56.9251 14.35819736 09
| Epoch (UTC): | 30 May 2026 10:32:46 |
| Eccentricity: | 0.0009974 |
| inclination: | 98.4172° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 330.8947° |
| argument of perigee: | 303.0977° |
| revolutions per day: | 14.35819736 |
| mean anomaly at epoch: | 56.9251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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