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 41188U 26087.70985427 +.00000000 +00000-0 +21172-3 0 00006
2 41188 47.0008 201.3189 0003585 205.3094 154.7617 14.58766807 04
| Epoch (UTC): | 28 March 2026 17:02:11 |
| Eccentricity: | 0.0003585 |
| inclination: | 47.0008° |
| perigee height: | 695 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 201.3189° |
| argument of perigee: | 205.3094° |
| revolutions per day: | 14.58766807 |
| mean anomaly at epoch: | 154.7617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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