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 26159.07706130 +.00000000 +00000-0 +00000-0 0 00005
2 41028 0.0491 113.5759 0004003 325.2533 298.9001 1.00271202 06
| Epoch (UTC): | 08 June 2026 01:50:58 |
| Eccentricity: | 0.0004003 |
| inclination: | 0.0491° |
| perigee height: | 35770 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 113.5759° |
| argument of perigee: | 325.2533° |
| revolutions per day: | 1.00271202 |
| mean anomaly at epoch: | 298.9001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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