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 37742U 26145.37844874 +.00000000 +00000-0 +16473-4 0 00004
2 37742 52.0130 262.6259 0000495 143.6498 252.0034 12.62263354 01
| Epoch (UTC): | 25 May 2026 09:04:57 |
| Eccentricity: | 0.0000495 |
| inclination: | 52.0130° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 262.6259° |
| argument of perigee: | 143.6498° |
| revolutions per day: | 12.62263354 |
| mean anomaly at epoch: | 252.0034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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