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 29047U 26106.18296792 +.00000000 +00000-0 +99832-4 0 00009
2 29047 71.9760 78.4609 0048910 342.9561 16.9931 14.31344587 09
| Epoch (UTC): | 16 April 2026 04:23:28 |
| Eccentricity: | 0.0048910 |
| inclination: | 71.9760° |
| perigee height: | 752 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 78.4609° |
| argument of perigee: | 342.9561° |
| revolutions per day: | 14.31344587 |
| mean anomaly at epoch: | 16.9931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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