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 65175U 26145.23441464 +.00000000 +00000-0 +36667-3 0 00004
2 65175 97.4488 17.6517 0002980 75.2983 284.8574 15.05662052 06
| Epoch (UTC): | 25 May 2026 05:37:33 |
| Eccentricity: | 0.0002980 |
| inclination: | 97.4488° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 17.6517° |
| argument of perigee: | 75.2983° |
| revolutions per day: | 15.05662052 |
| mean anomaly at epoch: | 284.8574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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