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 22626U 93024A 23156.48449998 .00001758 00000-0 17987-3 0 9994
2 22626 82.5196 145.6720 0020285 82.5102 277.8420 14.89845704630268
| Epoch (UTC): | 05 June 2023 11:37:40 |
| Eccentricity: | 0.0020285 |
| inclination: | 82.5196° |
| perigee height: | 584 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 145.6720° |
| argument of perigee: | 82.5102° |
| revolutions per day: | 14.89845704 |
| mean anomaly at epoch: | 277.8420° |
| orbit number at epoch: | 63026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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