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 38137U 26037.91311889 +.00000000 +00000-0 +44822-3 0 00006
2 38137 98.8574 84.4581 0044652 270.8108 88.7944 14.06224952 07
| Epoch (UTC): | 06 February 2026 21:54:53 |
| Eccentricity: | 0.0044652 |
| inclination: | 98.8574° |
| perigee height: | 840 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 84.4581° |
| argument of perigee: | 270.8108° |
| revolutions per day: | 14.06224952 |
| mean anomaly at epoch: | 88.7944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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