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 38466U 12033A 25049.88538066 0.00000000 00000-0 00000-0 0 03
2 38466 6.7157 83.9931 0005303 186.3128 173.6933 1.00270000 00
| Epoch (UTC): | 18 February 2025 21:14:56 |
| Eccentricity: | 0.0005303 |
| inclination: | 6.7157° |
| perigee height: | 35764 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 83.9931° |
| argument of perigee: | 186.3128° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 173.6933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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