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 26042.00910866 +.00000000 +00000-0 +16375-3 0 00008
2 37673 97.9835 57.0044 0001675 109.7604 272.7152 14.78382336 06
| Epoch (UTC): | 11 February 2026 00:13:06 |
| Eccentricity: | 0.0001675 |
| inclination: | 97.9835° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 57.0044° |
| argument of perigee: | 109.7604° |
| revolutions per day: | 14.78382336 |
| mean anomaly at epoch: | 272.7152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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