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 41028U 26113.51791222 +.00000000 +00000-0 +00000-0 0 00000
2 41028 0.0774 258.3675 0003570 138.7017 94.4442 1.00272491 06
| Epoch (UTC): | 23 April 2026 12:25:47 |
| Eccentricity: | 0.0003570 |
| inclination: | 0.0774° |
| perigee height: | 35771 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 258.3675° |
| argument of perigee: | 138.7017° |
| revolutions per day: | 1.00272491 |
| mean anomaly at epoch: | 94.4442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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