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 23705U 95058B 22148.83026102 .00000086 00000-0 68799-4 0 9990
2 23705 71.0208 198.4603 0010626 59.4666 300.7504 14.15171891372479
| Epoch (UTC): | 28 May 2022 19:55:34 |
| Eccentricity: | 0.0010626 |
| inclination: | 71.0208° |
| perigee height: | 834 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 198.4603° |
| argument of perigee: | 59.4666° |
| revolutions per day: | 14.15171891 |
| mean anomaly at epoch: | 300.7504° |
| orbit number at epoch: | 37247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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