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 21937U 26142.22105119 +.00000000 +00000-0 +31706-4 0 00002
2 21937 82.9301 134.4182 0032202 223.4437 147.3429 13.73386468 03
| Epoch (UTC): | 22 May 2026 05:18:18 |
| Eccentricity: | 0.0032202 |
| inclination: | 82.9301° |
| perigee height: | 964 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 134.4182° |
| argument of perigee: | 223.4437° |
| revolutions per day: | 13.73386468 |
| mean anomaly at epoch: | 147.3429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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