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 40074U 26036.90563741 +.00000000 +00000-0 +93613-3 0 00005
2 40074 98.4206 26.6631 0000751 132.1973 227.9318 15.11078730 04
| Epoch (UTC): | 05 February 2026 21:44:07 |
| Eccentricity: | 0.0000751 |
| inclination: | 98.4206° |
| perigee height: | 532 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 26.6631° |
| argument of perigee: | 132.1973° |
| revolutions per day: | 15.11078730 |
| mean anomaly at epoch: | 227.9318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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