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 23150.92806525 -.00000080 00000-0 -16597-4 0 9991
2 26070 71.0037 68.9672 0018915 283.1313 76.7699 14.15550026205086
| Epoch (UTC): | 30 May 2023 22:16:24 |
| Eccentricity: | 0.0018915 |
| inclination: | 71.0037° |
| perigee height: | 827 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 68.9672° |
| argument of perigee: | 283.1313° |
| revolutions per day: | 14.15550026 |
| mean anomaly at epoch: | 76.7699° |
| orbit number at epoch: | 20508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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