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 26129.81578340 +.00000000 +00000-0 +36720-3 0 00006
2 00051 47.2097 168.0910 0106241 82.9147 278.3709 12.18376991 00
| Epoch (UTC): | 09 May 2026 19:34:43 |
| Eccentricity: | 0.0106241 |
| inclination: | 47.2097° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 168.0910° |
| argument of perigee: | 82.9147° |
| revolutions per day: | 12.18376991 |
| mean anomaly at epoch: | 278.3709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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