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 12150U 81006B 25173.54395701 .00000017 00000-0 97274-4 0 9997
2 12150 65.8213 9.7507 0057699 217.1872 142.5190 13.77424922232008
| Epoch (UTC): | 22 June 2025 13:03:17 |
| Eccentricity: | 0.0057699 |
| inclination: | 65.8213° |
| perigee height: | 930 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 9.7507° |
| argument of perigee: | 217.1872° |
| revolutions per day: | 13.77424922 |
| mean anomaly at epoch: | 142.5190° |
| orbit number at epoch: | 23200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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