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 26133.34267823 +.00000000 +00000-0 +14152-4 0 00006
2 00051 47.2094 157.1767 0106173 93.3876 267.9064 12.18377091 05
| Epoch (UTC): | 13 May 2026 08:13:27 |
| Eccentricity: | 0.0106173 |
| inclination: | 47.2094° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 157.1767° |
| argument of perigee: | 93.3876° |
| revolutions per day: | 12.18377091 |
| mean anomaly at epoch: | 267.9064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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