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 13403U 26071.94797751 +.00000000 +00000-0 +29777-3 0 00004
2 13403 81.1477 189.2302 0025193 153.7775 206.4740 15.24852448 07
| Epoch (UTC): | 12 March 2026 22:45:05 |
| Eccentricity: | 0.0025193 |
| inclination: | 81.1477° |
| perigee height: | 474 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 189.2302° |
| argument of perigee: | 153.7775° |
| revolutions per day: | 15.24852448 |
| mean anomaly at epoch: | 206.4740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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