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 20441U 26155.03899242 +.00000000 +00000-0 +57503-4 0 00004
2 20441 98.8729 183.1453 0010082 258.2687 155.6135 14.33987556 07
| Epoch (UTC): | 04 June 2026 00:56:08 |
| Eccentricity: | 0.0010082 |
| inclination: | 98.8729° |
| perigee height: | 771 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 183.1453° |
| argument of perigee: | 258.2687° |
| revolutions per day: | 14.33987556 |
| mean anomaly at epoch: | 155.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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