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 23029.91493255 .00002127 00000-0 26890-3 0 9999
2 115 48.1665 351.6268 0033274 147.9180 212.3767 14.85253175355034
| Epoch (UTC): | 29 January 2023 21:57:30 |
| Eccentricity: | 0.0033274 |
| inclination: | 48.1665° |
| perigee height: | 589 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 351.6268° |
| argument of perigee: | 147.9180° |
| revolutions per day: | 14.85253175 |
| mean anomaly at epoch: | 212.3767° |
| orbit number at epoch: | 35503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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