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 66920U 26145.27964419 +.00000000 +00000-0 +63228-4 0 00001
2 66920 50.0100 228.0873 0000990 212.6284 147.4528 13.29325843 05
| Epoch (UTC): | 25 May 2026 06:42:41 |
| Eccentricity: | 0.0000990 |
| inclination: | 50.0100° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 228.0873° |
| argument of perigee: | 212.6284° |
| revolutions per day: | 13.29325843 |
| mean anomaly at epoch: | 147.4528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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