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 26074.58113691 +.00000000 +00000-0 +13528-3 0 00004
2 37673 97.9826 89.3018 0001977 82.0308 33.9101 14.78462409 05
| Epoch (UTC): | 15 March 2026 13:56:50 |
| Eccentricity: | 0.0001977 |
| inclination: | 97.9826° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 89.3018° |
| argument of perigee: | 82.0308° |
| revolutions per day: | 14.78462409 |
| mean anomaly at epoch: | 33.9101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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