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 26048.45081230 +.00000000 +00000-0 -63110-3 0 00007
2 00051 47.2137 59.8602 0110010 201.6886 157.9221 12.18378400 07
| Epoch (UTC): | 17 February 2026 10:49:10 |
| Eccentricity: | 0.0110010 |
| inclination: | 47.2137° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 59.8602° |
| argument of perigee: | 201.6886° |
| revolutions per day: | 12.18378400 |
| mean anomaly at epoch: | 157.9221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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