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 32283U 26014.53811043 +.00000000 +00000-0 +21076-3 0 00008
2 32283 98.1013 203.7852 0004085 147.7074 212.4478 16.47191300 06
| Epoch (UTC): | 14 January 2026 12:54:52 |
| Eccentricity: | 0.0004085 |
| inclination: | 98.1013° |
| perigee height: | 144 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 203.7852° |
| argument of perigee: | 147.7074° |
| revolutions per day: | 16.47191300 |
| mean anomaly at epoch: | 212.4478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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