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 is defined by the following mean orbital elements,
1 43941U 19004A 25303.69840922 0.00012000 00000-0 18631-3 0 06
2 43941 73.6190 269.3774 0014459 53.0552 306.9448 15.53722769 01
| Epoch (UTC): | 30 October 2025 16:45:42 |
| Eccentricity: | 0.0014459 |
| inclination: | 73.6190° |
| perigee height: | 396 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 269.3774° |
| argument of perigee: | 53.0552° |
| revolutions per day: | 15.53722769 |
| mean anomaly at epoch: | 306.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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