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 26040.54571274 +.00000000 +00000-0 +56162-3 0 00009
2 40057 98.2666 298.3653 0007576 347.0878 13.0147 14.96493520 02
| Epoch (UTC): | 09 February 2026 13:05:49 |
| Eccentricity: | 0.0007576 |
| inclination: | 98.2666° |
| perigee height: | 572 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 298.3653° |
| argument of perigee: | 347.0878° |
| revolutions per day: | 14.96493520 |
| mean anomaly at epoch: | 13.0147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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