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 12725U 26111.18107049 +.00000000 +00000-0 +10184-2 0 00007
2 12725 83.1409 16.0657 0088695 168.7691 313.6125 13.85477062 07
| Epoch (UTC): | 21 April 2026 04:20:44 |
| Eccentricity: | 0.0088695 |
| inclination: | 83.1409° |
| perigee height: | 880 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 16.0657° |
| argument of perigee: | 168.7691° |
| revolutions per day: | 13.85477062 |
| mean anomaly at epoch: | 313.6125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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