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 26104.21451155 +.00000000 +00000-0 +76895-4 0 00006
2 29709 98.1347 102.0017 0013134 39.1401 321.0761 14.85884762 05
| Epoch (UTC): | 14 April 2026 05:08:53 |
| Eccentricity: | 0.0013134 |
| inclination: | 98.1347° |
| perigee height: | 602 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 102.0017° |
| argument of perigee: | 39.1401° |
| revolutions per day: | 14.85884762 |
| mean anomaly at epoch: | 321.0761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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