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 26101.30910198 +.00000000 +00000-0 +30871-3 0 00002
2 40057 98.2578 2.5368 0008065 126.2205 233.9762 14.97276653 00
| Epoch (UTC): | 11 April 2026 07:25:06 |
| Eccentricity: | 0.0008065 |
| inclination: | 98.2578° |
| perigee height: | 570 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 2.5368° |
| argument of perigee: | 126.2205° |
| revolutions per day: | 14.97276653 |
| mean anomaly at epoch: | 233.9762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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