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 26065.28928433 +.00000000 +00000-0 +20524-3 0 00003
2 37673 97.9831 80.0878 0002011 90.3683 280.3788 14.78438805 03
| Epoch (UTC): | 06 March 2026 06:56:34 |
| Eccentricity: | 0.0002011 |
| inclination: | 97.9831° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 80.0878° |
| argument of perigee: | 90.3683° |
| revolutions per day: | 14.78438805 |
| mean anomaly at epoch: | 280.3788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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