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 26103.78983579 +.00000000 +00000-0 +14504-3 0 00009
2 39441 97.8853 43.4906 0064802 281.2686 78.1252 14.86393035 09
| Epoch (UTC): | 13 April 2026 18:57:21 |
| Eccentricity: | 0.0064802 |
| inclination: | 97.8853° |
| perigee height: | 564 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 43.4906° |
| argument of perigee: | 281.2686° |
| revolutions per day: | 14.86393035 |
| mean anomaly at epoch: | 78.1252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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