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 00205U 26019.83705625 +.00000000 +00000-0 +95306-5 0 00002
2 00205 32.4392 179.7619 0102401 288.1504 70.7989 13.62564807 00
| Epoch (UTC): | 19 January 2026 20:05:21 |
| Eccentricity: | 0.0102401 |
| inclination: | 32.4392° |
| perigee height: | 951 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 179.7619° |
| argument of perigee: | 288.1504° |
| revolutions per day: | 13.62564807 |
| mean anomaly at epoch: | 70.7989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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