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 23150.08008558 -.00000042 00000-0 32141-5 0 9999
2 26070 71.0037 70.7494 0018886 284.2691 75.6334 14.15550002204949
| Epoch (UTC): | 30 May 2023 01:55:19 |
| Eccentricity: | 0.0018886 |
| inclination: | 71.0037° |
| perigee height: | 827 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 70.7494° |
| argument of perigee: | 284.2691° |
| revolutions per day: | 14.15550002 |
| mean anomaly at epoch: | 75.6334° |
| orbit number at epoch: | 20494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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