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 61848U 26145.50391691 +.00000000 +00000-0 -20286-4 0 00005
2 61848 43.0010 153.0867 0001075 270.9838 89.0890 15.27570004 02
| Epoch (UTC): | 25 May 2026 12:05:38 |
| Eccentricity: | 0.0001075 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.0867° |
| argument of perigee: | 270.9838° |
| revolutions per day: | 15.27570004 |
| mean anomaly at epoch: | 89.0890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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