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 00446U 26135.23583566 +.00000000 +00000-0 -56154-5 0 00009
2 00446 50.1402 114.2794 0070224 277.7352 181.7302 13.35362410 04
| Epoch (UTC): | 15 May 2026 05:39:36 |
| Eccentricity: | 0.0070224 |
| inclination: | 50.1402° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 114.2794° |
| argument of perigee: | 277.7352° |
| revolutions per day: | 13.35362410 |
| mean anomaly at epoch: | 181.7302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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