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 28939U 06005A 23101.08243176 .21240275 30862-5 28003-3 0 9993
2 28939 98.1533 225.1159 0016560 270.3318 150.6016 16.48266844939525
| Epoch (UTC): | 11 April 2023 01:58:42 |
| Eccentricity: | 0.0016560 |
| inclination: | 98.1533° |
| perigee height: | 133 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 225.1159° |
| argument of perigee: | 270.3318° |
| revolutions per day: | 16.48266844 |
| mean anomaly at epoch: | 150.6016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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