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 39453U 26020.95513286 +.00000000 +00000-0 +46048-3 0 00001
2 39453 87.3362 109.3972 0002732 96.0982 264.0588 15.47515761 09
| Epoch (UTC): | 20 January 2026 22:55:23 |
| Eccentricity: | 0.0002732 |
| inclination: | 87.3362° |
| perigee height: | 422 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 109.3972° |
| argument of perigee: | 96.0982° |
| revolutions per day: | 15.47515761 |
| mean anomaly at epoch: | 264.0588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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