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 38773U 12048P 23295.73981622 0.00000000 00000-0 00000-0 0 05
2 38773 63.4298 158.3640 0229589 359.1213 0.8787 13.40770521 08
| Epoch (UTC): | 22 October 2023 17:45:20 |
| Eccentricity: | 0.0229589 |
| inclination: | 63.4298° |
| perigee height: | 934 km |
| apogee height: | 1278 km |
| right ascension of ascending node: | 158.3640° |
| argument of perigee: | 359.1213° |
| revolutions per day: | 13.40770521 |
| mean anomaly at epoch: | 0.8787° |
| 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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