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 25199.52021666 .00000026 00000-0 38852-4 0 9991
2 26069 70.9948 290.9776 0009253 73.4287 286.7850 14.13818689576791
| Epoch (UTC): | 18 July 2025 12:29:06 |
| Eccentricity: | 0.0009253 |
| inclination: | 70.9948° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 290.9776° |
| argument of perigee: | 73.4287° |
| revolutions per day: | 14.13818689 |
| mean anomaly at epoch: | 286.7850° |
| orbit number at epoch: | 57679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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