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 37152U 26145.56962917 +.00000000 +00000-0 +34845-4 0 00002
2 37152 82.4567 79.1693 0001182 111.7094 61.7985 12.42983831 09
| Epoch (UTC): | 25 May 2026 13:40:15 |
| Eccentricity: | 0.0001182 |
| inclination: | 82.4567° |
| perigee height: | 1493 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 79.1693° |
| argument of perigee: | 111.7094° |
| revolutions per day: | 12.42983831 |
| mean anomaly at epoch: | 61.7985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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