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 26071.29911272 +.00000000 +00000-0 +59788-3 0 00008
2 40057 98.2618 330.8417 0006282 229.3831 130.6843 14.96901113 04
| Epoch (UTC): | 12 March 2026 07:10:43 |
| Eccentricity: | 0.0006282 |
| inclination: | 98.2618° |
| perigee height: | 572 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 330.8417° |
| argument of perigee: | 229.3831° |
| revolutions per day: | 14.96901113 |
| mean anomaly at epoch: | 130.6843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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