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 65528U 26145.43636492 +.00000000 +00000-0 +34882-3 0 00002
2 65528 97.4484 215.1487 0001948 144.8203 215.3153 15.05662520 08
| Epoch (UTC): | 25 May 2026 10:28:21 |
| Eccentricity: | 0.0001948 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1487° |
| argument of perigee: | 144.8203° |
| revolutions per day: | 15.05662520 |
| mean anomaly at epoch: | 215.3153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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