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 26074.33457803 +.00000000 +00000-0 +25339-3 0 00002
2 29713 98.0289 103.9997 0020400 57.5484 302.7706 14.97953656 07
| Epoch (UTC): | 15 March 2026 08:01:47 |
| Eccentricity: | 0.0020400 |
| inclination: | 98.0289° |
| perigee height: | 559 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 103.9997° |
| argument of perigee: | 57.5484° |
| revolutions per day: | 14.97953656 |
| mean anomaly at epoch: | 302.7706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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