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 48274U 21035A 23030.15786262 .00014333 00000-0 16988-3 0 9990
2 48274 41.4749 277.4505 0002247 84.4155 49.2504 15.60936611100247
| Epoch (UTC): | 30 January 2023 03:47:19 |
| Eccentricity: | 0.0002247 |
| inclination: | 41.4749° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 277.4505° |
| argument of perigee: | 84.4155° |
| revolutions per day: | 15.60936611 |
| mean anomaly at epoch: | 49.2504° |
| orbit number at epoch: | 10024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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