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 04384U 70036B 22178.40483157 -.00000029 00000-0 -10158-3 0 9998
2 04384 74.0270 145.9633 0054128 279.9287 200.3973 12.39222816360005
| Epoch (UTC): | 27 June 2022 09:42:57 |
| Eccentricity: | 0.0054128 |
| inclination: | 74.0270° |
| perigee height: | 1467 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 145.9633° |
| argument of perigee: | 279.9287° |
| revolutions per day: | 12.39222816 |
| mean anomaly at epoch: | 200.3973° |
| orbit number at epoch: | 36000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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