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 00047U 26073.92564307 +.00000000 +00000-0 +11599-3 0 00006
2 00047 66.6646 299.9046 0222289 208.8557 150.0110 14.45197707 09
| Epoch (UTC): | 14 March 2026 22:12:55 |
| Eccentricity: | 0.0222289 |
| inclination: | 66.6646° |
| perigee height: | 583 km |
| apogee height: | 900 km |
| right ascension of ascending node: | 299.9046° |
| argument of perigee: | 208.8557° |
| revolutions per day: | 14.45197707 |
| mean anomaly at epoch: | 150.0110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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