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 25162.91508704 0.00000000 00000-0 00000-0 0 06
2 38773 63.4288 73.3765 0275244 358.2332 1.7668 13.40972861 01
| Epoch (UTC): | 11 June 2025 21:57:43 |
| Eccentricity: | 0.0275244 |
| inclination: | 63.4288° |
| perigee height: | 899 km |
| apogee height: | 1311 km |
| right ascension of ascending node: | 73.3765° |
| argument of perigee: | 358.2332° |
| revolutions per day: | 13.40972861 |
| mean anomaly at epoch: | 1.7668° |
| 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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