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 65538U 26145.14560559 +.00000000 +00000-0 +42964-3 0 00001
2 65538 97.4475 214.7679 0002380 132.4914 227.6514 15.05659921 08
| Epoch (UTC): | 25 May 2026 03:29:40 |
| Eccentricity: | 0.0002380 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.7679° |
| argument of perigee: | 132.4914° |
| revolutions per day: | 15.05659921 |
| mean anomaly at epoch: | 227.6514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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