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 26071.99660725 +.00000000 +00000-0 +25654-3 0 00000
2 29713 98.0297 101.5957 0020586 64.6752 295.6599 14.97939545 09
| Epoch (UTC): | 12 March 2026 23:55:06 |
| Eccentricity: | 0.0020586 |
| inclination: | 98.0297° |
| perigee height: | 559 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 101.5957° |
| argument of perigee: | 64.6752° |
| revolutions per day: | 14.97939545 |
| mean anomaly at epoch: | 295.6599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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