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 65174U 26145.23718160 +.00000000 +00000-0 +35014-3 0 00008
2 65174 97.4479 17.6506 0002392 78.6804 281.4692 15.05658309 03
| Epoch (UTC): | 25 May 2026 05:41:32 |
| Eccentricity: | 0.0002392 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6506° |
| argument of perigee: | 78.6804° |
| revolutions per day: | 15.05658309 |
| mean anomaly at epoch: | 281.4692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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