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 00051U 26046.07224626 +.00000000 +00000-0 -69444-3 0 00007
2 00051 47.2134 67.2204 0110103 194.6005 165.1592 12.18378604 00
| Epoch (UTC): | 15 February 2026 01:44:02 |
| Eccentricity: | 0.0110103 |
| inclination: | 47.2134° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 67.2204° |
| argument of perigee: | 194.6005° |
| revolutions per day: | 12.18378604 |
| mean anomaly at epoch: | 165.1592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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