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 00011U 26106.73303941 +.00000000 +00000-0 +39574-3 0 00001
2 00011 32.8668 317.7283 1444310 67.1492 307.4938 11.90352604 09
| Epoch (UTC): | 16 April 2026 17:35:34 |
| Eccentricity: | 0.1444310 |
| inclination: | 32.8668° |
| perigee height: | 554 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 317.7283° |
| argument of perigee: | 67.1492° |
| revolutions per day: | 11.90352604 |
| mean anomaly at epoch: | 307.4938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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