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 39440U 26072.31676753 +.00000000 +00000-0 +57111-3 0 00006
2 39440 97.8807 20.9950 0058193 346.9336 13.0372 14.93003467 09
| Epoch (UTC): | 13 March 2026 07:36:08 |
| Eccentricity: | 0.0058193 |
| inclination: | 97.8807° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 20.9950° |
| argument of perigee: | 346.9336° |
| revolutions per day: | 14.93003467 |
| mean anomaly at epoch: | 13.0372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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