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 43245U 26145.39635957 +.00000000 +00000-0 +00000-0 0 00006
2 43245 54.2150 300.7449 0000920 121.0024 238.9826 1.86228327 02
| Epoch (UTC): | 25 May 2026 09:30:45 |
| Eccentricity: | 0.0000920 |
| inclination: | 54.2150° |
| perigee height: | 21526 km |
| apogee height: | 21531 km |
| right ascension of ascending node: | 300.7449° |
| argument of perigee: | 121.0024° |
| revolutions per day: | 1.86228327 |
| mean anomaly at epoch: | 238.9826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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