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 40071U 26044.91177434 +.00000000 +00000-0 +18419-3 0 00003
2 40071 98.3714 359.2885 0006429 325.1819 34.8976 14.89503109 03
| Epoch (UTC): | 13 February 2026 21:52:57 |
| Eccentricity: | 0.0006429 |
| inclination: | 98.3714° |
| perigee height: | 595 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 359.2885° |
| argument of perigee: | 325.1819° |
| revolutions per day: | 14.89503109 |
| mean anomaly at epoch: | 34.8976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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