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 29479U 26145.29282010 +.00000000 +00000-0 +12249-3 0 00007
2 29479 98.0554 161.7830 0017503 5.8763 354.2644 14.68583925 04
| Epoch (UTC): | 25 May 2026 07:01:39 |
| Eccentricity: | 0.0017503 |
| inclination: | 98.0554° |
| perigee height: | 653 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 161.7830° |
| argument of perigee: | 5.8763° |
| revolutions per day: | 14.68583925 |
| mean anomaly at epoch: | 354.2644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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