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 53170U 26145.35811844 +.00000000 +00000-0 +43609-4 0 00007
2 53170 53.2128 174.8949 0001019 75.9401 284.1705 15.08853585 03
| Epoch (UTC): | 25 May 2026 08:35:41 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.8949° |
| argument of perigee: | 75.9401° |
| revolutions per day: | 15.08853585 |
| mean anomaly at epoch: | 284.1705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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