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 65664U 26145.38474065 +.00000000 +00000-0 +20419-3 0 00004
2 65664 97.4474 189.3138 0001947 127.4723 232.6681 15.05659198 01
| Epoch (UTC): | 25 May 2026 09:14:01 |
| Eccentricity: | 0.0001947 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.3138° |
| argument of perigee: | 127.4723° |
| revolutions per day: | 15.05659198 |
| mean anomaly at epoch: | 232.6681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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