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 29709U 26030.20392609 +.00000000 +00000-0 -97047-3 0 00003
2 29709 98.1291 26.3713 0010744 275.7228 84.2761 14.85761776 00
| Epoch (UTC): | 30 January 2026 04:53:39 |
| Eccentricity: | 0.0010744 |
| inclination: | 98.1291° |
| perigee height: | 604 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 26.3713° |
| argument of perigee: | 275.7228° |
| revolutions per day: | 14.85761776 |
| mean anomaly at epoch: | 84.2761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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