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 38466U 12033A 23059.89446220 0.00000000 00000-0 00000-0 0 03
2 38466 4.8752 96.6159 0004263 176.2274 183.7726 1.00270000 09
| Epoch (UTC): | 28 February 2023 21:28:01 |
| Eccentricity: | 0.0004263 |
| inclination: | 4.8752° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 96.6159° |
| argument of perigee: | 176.2274° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 183.7726° |
| 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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