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 26072.93179872 +.00000000 +00000-0 +24551-3 0 00008
2 29713 98.0295 102.5573 0020524 61.7958 298.5333 14.97944583 06
| Epoch (UTC): | 13 March 2026 22:21:47 |
| Eccentricity: | 0.0020524 |
| inclination: | 98.0295° |
| perigee height: | 559 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 102.5573° |
| argument of perigee: | 61.7958° |
| revolutions per day: | 14.97944583 |
| mean anomaly at epoch: | 298.5333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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