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 26145.48696845 +.00000000 +00000-0 +82262-3 0 00001
2 37818 62.8260 135.3385 4624630 283.0670 30.7635 6.15448564 09
| Epoch (UTC): | 25 May 2026 11:41:14 |
| Eccentricity: | 0.4624630 |
| inclination: | 62.8260° |
| perigee height: | 383 km |
| apogee height: | 12017 km |
| right ascension of ascending node: | 135.3385° |
| argument of perigee: | 283.0670° |
| revolutions per day: | 6.15448564 |
| mean anomaly at epoch: | 30.7635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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