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 26071.12821213 +.00000000 +00000-0 +25122-3 0 00006
2 29713 98.0300 100.7028 0020660 67.3560 292.9843 14.97934414 06
| Epoch (UTC): | 12 March 2026 03:04:37 |
| Eccentricity: | 0.0020660 |
| inclination: | 98.0300° |
| perigee height: | 559 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 100.7028° |
| argument of perigee: | 67.3560° |
| revolutions per day: | 14.97934414 |
| mean anomaly at epoch: | 292.9843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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