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 39420U 26145.37516295 +.00000000 +00000-0 +18634-3 0 00002
2 39420 97.6837 11.4803 0118206 85.1148 276.3545 14.72256626 05
| Epoch (UTC): | 25 May 2026 09:00:14 |
| Eccentricity: | 0.0118206 |
| inclination: | 97.6837° |
| perigee height: | 571 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 11.4803° |
| argument of perigee: | 85.1148° |
| revolutions per day: | 14.72256626 |
| mean anomaly at epoch: | 276.3545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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