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 26042.16739962 +.00000000 +00000-0 +28094-4 0 00001
2 07575 81.2452 111.5353 0048941 307.8251 51.8495 14.11555693 01
| Epoch (UTC): | 11 February 2026 04:01:03 |
| Eccentricity: | 0.0048941 |
| inclination: | 81.2452° |
| perigee height: | 819 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 111.5353° |
| argument of perigee: | 307.8251° |
| revolutions per day: | 14.11555693 |
| mean anomaly at epoch: | 51.8495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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