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 38109U 12014A 23030.21017461 0.00000000 00000-0 00000-0 0 02
2 38109 122.9981 246.3761 0007384 212.0207 147.9793 13.41440008 05
| Epoch (UTC): | 30 January 2023 05:02:39 |
| Eccentricity: | 0.0007384 |
| inclination: | 122.9981° |
| perigee height: | 1098 km |
| apogee height: | 1109 km |
| right ascension of ascending node: | 246.3761° |
| argument of perigee: | 212.0207° |
| revolutions per day: | 13.41440008 |
| mean anomaly at epoch: | 147.9793° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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