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 26083.73555581 +.00000000 +00000-0 +35306-4 0 00009
2 00205 32.4396 220.3817 0101769 52.3472 308.6332 13.62569151 00
| Epoch (UTC): | 24 March 2026 17:39:12 |
| Eccentricity: | 0.0101769 |
| inclination: | 32.4396° |
| perigee height: | 951 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 220.3817° |
| argument of perigee: | 52.3472° |
| revolutions per day: | 13.62569151 |
| mean anomaly at epoch: | 308.6332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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