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 data is extracted from the following two-line orbital elements,
1 26069U 00006A 25198.45894402 -.00000002 00000-0 24065-4 0 9994
2 26069 70.9949 293.2025 0009219 75.2892 284.9251 14.13818561576647
| Epoch (UTC): | 17 July 2025 11:00:52 |
| Eccentricity: | 0.0009219 |
| inclination: | 70.9949° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 293.2025° |
| argument of perigee: | 75.2892° |
| revolutions per day: | 14.13818561 |
| mean anomaly at epoch: | 284.9251° |
| orbit number at epoch: | 57664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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