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 23030.92402072 .00001967 00000-0 25059-3 0 9996
2 115 48.1668 346.7619 0033310 152.3289 207.9406 14.85257723355182
| Epoch (UTC): | 30 January 2023 22:10:35 |
| Eccentricity: | 0.0033310 |
| inclination: | 48.1668° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 346.7619° |
| argument of perigee: | 152.3289° |
| revolutions per day: | 14.85257723 |
| mean anomaly at epoch: | 207.9406° |
| orbit number at epoch: | 35518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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