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 26074.97596229 +.00000000 +00000-0 +13498-3 0 00005
2 37673 97.9825 89.6933 0001963 81.7362 334.3766 14.78463375 02
| Epoch (UTC): | 15 March 2026 23:25:23 |
| Eccentricity: | 0.0001963 |
| inclination: | 97.9825° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 89.6933° |
| argument of perigee: | 81.7362° |
| revolutions per day: | 14.78463375 |
| mean anomaly at epoch: | 334.3766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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