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 46171U 26144.99101485 +.00000000 +00000-0 +72974-3 0 00008
2 46171 53.0341 242.8267 0004994 284.6948 75.3517 15.76537285 02
| Epoch (UTC): | 24 May 2026 23:47:03 |
| Eccentricity: | 0.0004994 |
| inclination: | 53.0341° |
| perigee height: | 337 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 242.8267° |
| argument of perigee: | 284.6948° |
| revolutions per day: | 15.76537285 |
| mean anomaly at epoch: | 75.3517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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