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 38770U 12048N 23002.25272022 0.00010600 00000-0 59382-3 0 09
2 38770 64.6384 103.9911 0157656 210.5361 149.4639 15.03088100 02
| Epoch (UTC): | 02 January 2023 06:03:55 |
| Eccentricity: | 0.0157656 |
| inclination: | 64.6384° |
| perigee height: | 448 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 103.9911° |
| argument of perigee: | 210.5361° |
| revolutions per day: | 15.03088100 |
| mean anomaly at epoch: | 149.4639° |
| 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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