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 01292U 26153.80858575 +.00000000 +00000-0 +98879-4 0 00005
2 01292 70.0777 342.5710 0020764 322.6201 37.3463 14.01583384 04
| Epoch (UTC): | 02 June 2026 19:24:21 |
| Eccentricity: | 0.0020764 |
| inclination: | 70.0777° |
| perigee height: | 873 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 342.5710° |
| argument of perigee: | 322.6201° |
| revolutions per day: | 14.01583384 |
| mean anomaly at epoch: | 37.3463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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