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 01208U 26153.32259633 +.00000000 +00000-0 +84737-4 0 00007
2 01208 70.0790 215.7617 0017654 107.5873 323.0653 13.96078101 07
| Epoch (UTC): | 02 June 2026 07:44:32 |
| Eccentricity: | 0.0017654 |
| inclination: | 70.0790° |
| perigee height: | 895 km |
| apogee height: | 920 km |
| right ascension of ascending node: | 215.7617° |
| argument of perigee: | 107.5873° |
| revolutions per day: | 13.96078101 |
| mean anomaly at epoch: | 323.0653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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