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 41915U 17002C 23332.11667670 .00015371 00000-0 65760-3 0 9991
2 41915 97.2268 2.0871 0006398 221.7750 138.3000 15.22887033380065
| Epoch (UTC): | 28 November 2023 02:48:00 |
| Eccentricity: | 0.0006398 |
| inclination: | 97.2268° |
| perigee height: | 493 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 2.0871° |
| argument of perigee: | 221.7750° |
| revolutions per day: | 15.22887033 |
| mean anomaly at epoch: | 138.3000° |
| orbit number at epoch: | 38006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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