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 61733U 26145.61230616 +.00000000 +00000-0 +00000-0 0 00006
2 61733 0.0154 289.2323 0000369 205.7288 112.7374 1.00271712 07
| Epoch (UTC): | 25 May 2026 14:41:43 |
| Eccentricity: | 0.0000369 |
| inclination: | 0.0154° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 289.2323° |
| argument of perigee: | 205.7288° |
| revolutions per day: | 1.00271712 |
| mean anomaly at epoch: | 112.7374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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