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 23037.18027885 .00002958 00000-0 36313-3 0 9992
2 00115 48.1667 316.5993 0033644 180.0578 180.0337 14.85295077334950
| Epoch (UTC): | 06 February 2023 04:19:36 |
| Eccentricity: | 0.0033644 |
| inclination: | 48.1667° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 316.5993° |
| argument of perigee: | 180.0578° |
| revolutions per day: | 14.85295077 |
| mean anomaly at epoch: | 180.0337° |
| orbit number at epoch: | 33495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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