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 07369U 74054A 23341.52550003 .00000035 00000-0 00000-0 0 9996
2 07369 124.7464 144.4116 0066454 20.7899 32.7685 3.07214724554270
| Epoch (UTC): | 07 December 2023 12:36:43 |
| Eccentricity: | 0.0066454 |
| inclination: | 124.7464° |
| perigee height: | 13477 km |
| apogee height: | 13743 km |
| right ascension of ascending node: | 144.4116° |
| argument of perigee: | 20.7899° |
| revolutions per day: | 3.07214724 |
| mean anomaly at epoch: | 32.7685° |
| orbit number at epoch: | 55427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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