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 26031.37546234 +.00000000 +00000-0 +89439-3 0 00002
2 37818 62.8253 213.3630 4633318 279.5631 32.7380 6.14852044 01
| Epoch (UTC): | 31 January 2026 09:00:39 |
| Eccentricity: | 0.4633318 |
| inclination: | 62.8253° |
| perigee height: | 376 km |
| apogee height: | 12039 km |
| right ascension of ascending node: | 213.3630° |
| argument of perigee: | 279.5631° |
| revolutions per day: | 6.14852044 |
| mean anomaly at epoch: | 32.7380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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