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 53166U 26145.66668980 +.00000000 +00000-0 +24430-2 0 00006
2 53166 53.2173 171.4319 0001503 61.0518 22.4475 15.42992999 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001503 |
| inclination: | 53.2173° |
| perigee height: | 436 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 171.4319° |
| argument of perigee: | 61.0518° |
| revolutions per day: | 15.42992999 |
| mean anomaly at epoch: | 22.4475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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