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 55976U 26145.60419603 +.00000000 +00000-0 +28735-3 0 00000
2 55976 97.5219 318.9394 0003369 170.8439 189.2873 15.47036724 04
| Epoch (UTC): | 25 May 2026 14:30:02 |
| Eccentricity: | 0.0003369 |
| inclination: | 97.5219° |
| perigee height: | 423 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 318.9394° |
| argument of perigee: | 170.8439° |
| revolutions per day: | 15.47036724 |
| mean anomaly at epoch: | 189.2873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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