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 115U 60002D 22332.27624447 .00001399 00000-0 18716-3 0 9991
2 115 48.1669 293.5396 0034066 231.3257 128.4607 14.84940373345724
| Epoch (UTC): | 28 November 2022 06:37:47 |
| Eccentricity: | 0.0034066 |
| inclination: | 48.1669° |
| perigee height: | 590 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 293.5396° |
| argument of perigee: | 231.3257° |
| revolutions per day: | 14.84940373 |
| mean anomaly at epoch: | 128.4607° |
| orbit number at epoch: | 34572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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