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 40012U 26156.70319073 +.00000000 +00000-0 +43462-3 0 00002
2 40012 97.7873 309.6189 0046454 106.0536 254.5803 14.88181134 06
| Epoch (UTC): | 05 June 2026 16:52:35 |
| Eccentricity: | 0.0046454 |
| inclination: | 97.7873° |
| perigee height: | 571 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 309.6189° |
| argument of perigee: | 106.0536° |
| revolutions per day: | 14.88181134 |
| mean anomaly at epoch: | 254.5803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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