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 12646U 26157.09277801 +.00000000 +00000-0 +10536-4 0 00006
2 12646 81.2261 284.7952 0066725 353.2696 179.6117 14.16425870 08
| Epoch (UTC): | 06 June 2026 02:13:36 |
| Eccentricity: | 0.0066725 |
| inclination: | 81.2261° |
| perigee height: | 789 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 284.7952° |
| argument of perigee: | 353.2696° |
| revolutions per day: | 14.16425870 |
| mean anomaly at epoch: | 179.6117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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