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 37225U 26077.78613513 +.00000000 +00000-0 +85476-4 0 00002
2 37225 71.9747 0.7611 0018499 294.5175 65.4060 14.82036934 06
| Epoch (UTC): | 18 March 2026 18:52:02 |
| Eccentricity: | 0.0018499 |
| inclination: | 71.9747° |
| perigee height: | 610 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 0.7611° |
| argument of perigee: | 294.5175° |
| revolutions per day: | 14.82036934 |
| mean anomaly at epoch: | 65.4060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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