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 48501U 94074EC 23128.67511329 .26070317 27423-5 81353-2 0 9993
2 48501 97.8361 190.5464 0019573 272.9043 87.0007 16.26016355117955
| Epoch (UTC): | 08 May 2023 16:12:09 |
| Eccentricity: | 0.0019573 |
| inclination: | 97.8361° |
| perigee height: | 190 km |
| apogee height: | 216 km |
| right ascension of ascending node: | 190.5464° |
| argument of perigee: | 272.9043° |
| revolutions per day: | 16.26016355 |
| mean anomaly at epoch: | 87.0007° |
| orbit number at epoch: | 11795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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