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 37673U 26017.98773167 +.00000000 +00000-0 +12239-3 0 00003
2 37673 97.9832 33.1899 0000909 106.3710 310.7688 14.78301886 04
| Epoch (UTC): | 17 January 2026 23:42:20 |
| Eccentricity: | 0.0000909 |
| inclination: | 97.9832° |
| perigee height: | 634 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 33.1899° |
| argument of perigee: | 106.3710° |
| revolutions per day: | 14.78301886 |
| mean anomaly at epoch: | 310.7688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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