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 39301U 92093JS 24350.99426372 .00000781 00000-0 45566-3 0 9990
2 39301 70.8821 255.6350 0032275 21.7793 338.4690 14.11378541148122
| Epoch (UTC): | 15 December 2024 23:51:44 |
| Eccentricity: | 0.0032275 |
| inclination: | 70.8821° |
| perigee height: | 831 km |
| apogee height: | 878 km |
| right ascension of ascending node: | 255.6350° |
| argument of perigee: | 21.7793° |
| revolutions per day: | 14.11378541 |
| mean anomaly at epoch: | 338.4690° |
| orbit number at epoch: | 14812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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