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 26103.07401962 +.00000000 +00000-0 +62957-3 0 00003
2 37818 62.8205 164.3466 4625867 281.7685 31.5264 6.15289786 00
| Epoch (UTC): | 13 April 2026 01:46:35 |
| Eccentricity: | 0.4625867 |
| inclination: | 62.8205° |
| perigee height: | 383 km |
| apogee height: | 12021 km |
| right ascension of ascending node: | 164.3466° |
| argument of perigee: | 281.7685° |
| revolutions per day: | 6.15289786 |
| mean anomaly at epoch: | 31.5264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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