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 39441U 26160.06484735 +.00000000 +00000-0 +20686-3 0 00001
2 39441 97.8887 99.3379 0067700 96.1920 264.7013 14.86583594 03
| Epoch (UTC): | 09 June 2026 01:33:22 |
| Eccentricity: | 0.0067700 |
| inclination: | 97.8887° |
| perigee height: | 561 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 99.3379° |
| argument of perigee: | 96.1920° |
| revolutions per day: | 14.86583594 |
| mean anomaly at epoch: | 264.7013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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