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 26064.63177435 +.00000000 +00000-0 +20892-3 0 00007
2 37673 97.9830 79.4358 0002026 91.1740 22.1829 14.78437185 04
| Epoch (UTC): | 05 March 2026 15:09:45 |
| Eccentricity: | 0.0002026 |
| inclination: | 97.9830° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 79.4358° |
| argument of perigee: | 91.1740° |
| revolutions per day: | 14.78437185 |
| mean anomaly at epoch: | 22.1829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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