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 26075.24294544 +.00000000 +00000-0 +46869-3 0 00009
2 40057 98.2617 335.0066 0006732 213.9122 146.1669 14.96948828 04
| Epoch (UTC): | 16 March 2026 05:49:50 |
| Eccentricity: | 0.0006732 |
| inclination: | 98.2617° |
| perigee height: | 572 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 335.0066° |
| argument of perigee: | 213.9122° |
| revolutions per day: | 14.96948828 |
| mean anomaly at epoch: | 146.1669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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