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 53173U 26145.43724411 +.00000000 +00000-0 +12643-3 0 00005
2 53173 53.2124 154.5770 0001227 92.2932 267.8201 15.08835164 03
| Epoch (UTC): | 25 May 2026 10:29:37 |
| Eccentricity: | 0.0001227 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.5770° |
| argument of perigee: | 92.2932° |
| revolutions per day: | 15.08835164 |
| mean anomaly at epoch: | 267.8201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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