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 57065U 26145.40080456 +.00000000 +00000-0 +61511-4 0 00009
2 57065 43.0036 40.8732 0000885 257.3985 102.6767 15.26748808 03
| Epoch (UTC): | 25 May 2026 09:37:09 |
| Eccentricity: | 0.0000885 |
| inclination: | 43.0036° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 40.8732° |
| argument of perigee: | 257.3985° |
| revolutions per day: | 15.26748808 |
| mean anomaly at epoch: | 102.6767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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