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 40072U 26032.40862788 +.00000000 +00000-0 +23267-3 0 00005
2 40072 98.3673 343.8159 0005905 13.3631 346.7739 14.87566555 01
| Epoch (UTC): | 01 February 2026 09:48:25 |
| Eccentricity: | 0.0005905 |
| inclination: | 98.3673° |
| perigee height: | 601 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 343.8159° |
| argument of perigee: | 13.3631° |
| revolutions per day: | 14.87566555 |
| mean anomaly at epoch: | 346.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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