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 27437U 26022.19168602 +.00000000 +00000-0 +12082-3 0 00007
2 27437 82.9480 258.3906 0042565 233.2005 126.5244 13.76932104 06
| Epoch (UTC): | 22 January 2026 04:36:01 |
| Eccentricity: | 0.0042565 |
| inclination: | 82.9480° |
| perigee height: | 943 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 258.3906° |
| argument of perigee: | 233.2005° |
| revolutions per day: | 13.76932104 |
| mean anomaly at epoch: | 126.5244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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