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 39416U 26032.42360433 +.00000000 +00000-0 +22097-3 0 00007
2 39416 97.7541 347.7723 0034717 303.0178 56.7706 14.91139692 01
| Epoch (UTC): | 01 February 2026 10:09:59 |
| Eccentricity: | 0.0034717 |
| inclination: | 97.7541° |
| perigee height: | 570 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 347.7723° |
| argument of perigee: | 303.0178° |
| revolutions per day: | 14.91139692 |
| mean anomaly at epoch: | 56.7706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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