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 26053.70459641 +.00000000 +00000-0 +99960-4 0 00002
2 37154 82.4625 133.9331 0014841 193.0841 283.7327 12.43743168 07
| Epoch (UTC): | 22 February 2026 16:54:37 |
| Eccentricity: | 0.0014841 |
| inclination: | 82.4625° |
| perigee height: | 1479 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 133.9331° |
| argument of perigee: | 193.0841° |
| revolutions per day: | 12.43743168 |
| mean anomaly at epoch: | 283.7327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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