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 29713U 26040.26458006 +.00000000 +00000-0 +25309-3 0 00000
2 29713 98.0333 68.9617 0020144 166.8279 193.3472 14.97733808 06
| Epoch (UTC): | 09 February 2026 06:20:59 |
| Eccentricity: | 0.0020144 |
| inclination: | 98.0333° |
| perigee height: | 560 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 68.9617° |
| argument of perigee: | 166.8279° |
| revolutions per day: | 14.97733808 |
| mean anomaly at epoch: | 193.3472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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