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 00050U 60009B 22269.71198597 -.00000072 00000-0 12130-3 0 9998
2 00050 47.2323 61.3083 0113450 283.0437 75.7709 12.20122228771710
| Epoch (UTC): | 26 September 2022 17:05:15 |
| Eccentricity: | 0.0113450 |
| inclination: | 47.2323° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 61.3083° |
| argument of perigee: | 283.0437° |
| revolutions per day: | 12.20122228 |
| mean anomaly at epoch: | 75.7709° |
| orbit number at epoch: | 77171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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