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 37154U 26160.20824830 +.00000000 +00000-0 +31530-4 0 00001
2 37154 82.4613 67.2340 0014410 330.5594 142.1410 12.43747145 08
| Epoch (UTC): | 09 June 2026 04:59:52 |
| Eccentricity: | 0.0014410 |
| inclination: | 82.4613° |
| perigee height: | 1479 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 67.2340° |
| argument of perigee: | 330.5594° |
| revolutions per day: | 12.43747145 |
| mean anomaly at epoch: | 142.1410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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