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 40057U 26038.20545906 +.00000000 +00000-0 +67342-3 0 00004
2 40057 98.2670 295.8943 0007627 355.5808 4.5343 14.96464533 00
| Epoch (UTC): | 07 February 2026 04:55:51 |
| Eccentricity: | 0.0007627 |
| inclination: | 98.2670° |
| perigee height: | 573 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 295.8943° |
| argument of perigee: | 355.5808° |
| revolutions per day: | 14.96464533 |
| mean anomaly at epoch: | 4.5343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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