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 40056U 26071.21024007 +.00000000 +00000-0 +18256-3 0 00005
2 40056 98.3275 302.9324 0012143 328.3215 31.7264 14.81085890 06
| Epoch (UTC): | 12 March 2026 05:02:44 |
| Eccentricity: | 0.0012143 |
| inclination: | 98.3275° |
| perigee height: | 617 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 302.9324° |
| argument of perigee: | 328.3215° |
| revolutions per day: | 14.81085890 |
| mean anomaly at epoch: | 31.7264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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