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 26021.49051600 +.00000000 +00000-0 +58192-3 0 00009
2 29713 98.0354 49.6533 0018498 227.4650 132.5010 14.97590917 03
| Epoch (UTC): | 21 January 2026 11:46:20 |
| Eccentricity: | 0.0018498 |
| inclination: | 98.0354° |
| perigee height: | 561 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 49.6533° |
| argument of perigee: | 227.4650° |
| revolutions per day: | 14.97590917 |
| mean anomaly at epoch: | 132.5010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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