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 13066U 26158.90636983 +.00000000 +00000-0 +98620-4 0 00004
2 13066 82.8967 287.3276 0044759 67.3213 49.9346 13.77398889 02
| Epoch (UTC): | 07 June 2026 21:45:10 |
| Eccentricity: | 0.0044759 |
| inclination: | 82.8967° |
| perigee height: | 940 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 287.3276° |
| argument of perigee: | 67.3213° |
| revolutions per day: | 13.77398889 |
| mean anomaly at epoch: | 49.9346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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