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 26140.72452292 +.00000000 +00000-0 -13245-3 0 00004
2 00051 47.2095 134.3331 0106137 115.3020 245.8808 12.18376748 05
| Epoch (UTC): | 20 May 2026 17:23:18 |
| Eccentricity: | 0.0106137 |
| inclination: | 47.2095° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 134.3331° |
| argument of perigee: | 115.3020° |
| revolutions per day: | 12.18376748 |
| mean anomaly at epoch: | 245.8808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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