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 04071U 69070B 23331.89223556 .00001739 00000-0 33648-3 0 9993
2 04071 74.0481 290.1311 0013740 17.9024 342.2625 14.64084420882154
| Epoch (UTC): | 27 November 2023 21:24:49 |
| Eccentricity: | 0.0013740 |
| inclination: | 74.0481° |
| perigee height: | 670 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 290.1311° |
| argument of perigee: | 17.9024° |
| revolutions per day: | 14.64084420 |
| mean anomaly at epoch: | 342.2625° |
| orbit number at epoch: | 88215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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