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 23704U 95058A 23089.83947747 .00000068 00000-0 61262-4 0 9999
2 23704 70.9832 295.4321 0008601 148.6794 211.4841 14.13502565414155
| Epoch (UTC): | 30 March 2023 20:08:50 |
| Eccentricity: | 0.0008601 |
| inclination: | 70.9832° |
| perigee height: | 841 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 295.4321° |
| argument of perigee: | 148.6794° |
| revolutions per day: | 14.13502565 |
| mean anomaly at epoch: | 211.4841° |
| orbit number at epoch: | 41415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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