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 07575U 26039.33207323 +.00000000 +00000-0 -36090-5 0 00004
2 07575 81.2458 114.3017 0049150 315.9635 43.7626 14.11555625 05
| Epoch (UTC): | 08 February 2026 07:58:11 |
| Eccentricity: | 0.0049150 |
| inclination: | 81.2458° |
| perigee height: | 819 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 114.3017° |
| argument of perigee: | 315.9635° |
| revolutions per day: | 14.11555625 |
| mean anomaly at epoch: | 43.7626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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