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 26071.23696056 +.00000000 +00000-0 +74874-4 0 00006
2 13066 82.9017 352.9661 0042632 313.1913 211.8534 13.77379674 03
| Epoch (UTC): | 12 March 2026 05:41:13 |
| Eccentricity: | 0.0042632 |
| inclination: | 82.9017° |
| perigee height: | 942 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 352.9661° |
| argument of perigee: | 313.1913° |
| revolutions per day: | 13.77379674 |
| mean anomaly at epoch: | 211.8534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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