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 05051U 26088.15837005 +.00000000 +00000-0 +12271-3 0 00003
2 05051 65.8137 132.6974 0043892 147.1846 213.1956 13.76117400 09
| Epoch (UTC): | 29 March 2026 03:48:03 |
| Eccentricity: | 0.0043892 |
| inclination: | 65.8137° |
| perigee height: | 945 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 132.6974° |
| argument of perigee: | 147.1846° |
| revolutions per day: | 13.76117400 |
| mean anomaly at epoch: | 213.1956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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