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 37818U 26160.27191862 +.00000000 +00000-0 +79215-3 0 00008
2 37818 62.8229 125.2216 4622556 283.4970 30.5389 6.15518657 02
| Epoch (UTC): | 09 June 2026 06:31:33 |
| Eccentricity: | 0.4622556 |
| inclination: | 62.8229° |
| perigee height: | 385 km |
| apogee height: | 12013 km |
| right ascension of ascending node: | 125.2216° |
| argument of perigee: | 283.4970° |
| revolutions per day: | 6.15518657 |
| mean anomaly at epoch: | 30.5389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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