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 26070U 00006B 25191.60365457 .00000084 00000-0 67008-4 0 9992
2 26070 71.0016 246.8384 0017056 197.7237 162.3293 14.15781345314296
| Epoch (UTC): | 10 July 2025 14:29:15 |
| Eccentricity: | 0.0017056 |
| inclination: | 71.0016° |
| perigee height: | 827 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 246.8384° |
| argument of perigee: | 197.7237° |
| revolutions per day: | 14.15781345 |
| mean anomaly at epoch: | 162.3293° |
| orbit number at epoch: | 31429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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