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 06966U 73098B 25194.61451488 .00000186 00000-0 61265-4 0 9991
2 06966 74.0547 150.9533 0019533 103.5106 256.8230 14.44605109710568
| Epoch (UTC): | 13 July 2025 14:44:54 |
| Eccentricity: | 0.0019533 |
| inclination: | 74.0547° |
| perigee height: | 729 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 150.9533° |
| argument of perigee: | 103.5106° |
| revolutions per day: | 14.44605109 |
| mean anomaly at epoch: | 256.8230° |
| orbit number at epoch: | 71056 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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