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 39452U 26079.96468671 +.00000000 +00000-0 +19972-3 0 00008
2 39452 87.3278 88.9766 0003274 95.1886 264.9748 15.49001370 07
| Epoch (UTC): | 20 March 2026 23:09:08 |
| Eccentricity: | 0.0003274 |
| inclination: | 87.3278° |
| perigee height: | 417 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 88.9766° |
| argument of perigee: | 95.1886° |
| revolutions per day: | 15.49001370 |
| mean anomaly at epoch: | 264.9748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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