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 00115U 60002D 23030.25129562 .00002068 00000-0 26215-3 0 9990
2 00115 48.1665 350.0052 0033285 149.4627 210.8233 14.85254720333925
| Epoch (UTC): | 30 January 2023 06:01:51 |
| Eccentricity: | 0.0033285 |
| inclination: | 48.1665° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 350.0052° |
| argument of perigee: | 149.4627° |
| revolutions per day: | 14.85254720 |
| mean anomaly at epoch: | 210.8233° |
| orbit number at epoch: | 33392 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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