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 23154.74397540 -.00000190 00000-0 -72494-4 0 9997
2 26070 71.0037 60.9478 0018927 277.9617 81.9358 14.15549440205609
| Epoch (UTC): | 03 June 2023 17:51:19 |
| Eccentricity: | 0.0018927 |
| inclination: | 71.0037° |
| perigee height: | 827 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 60.9478° |
| argument of perigee: | 277.9617° |
| revolutions per day: | 14.15549440 |
| mean anomaly at epoch: | 81.9358° |
| orbit number at epoch: | 20560 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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