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 14781U 26150.83698024 +.00000000 +00000-0 +16069-3 0 00003
2 14781 97.8048 116.6072 0006231 234.9595 125.1039 14.90736305 00
| Epoch (UTC): | 30 May 2026 20:05:15 |
| Eccentricity: | 0.0006231 |
| inclination: | 97.8048° |
| perigee height: | 591 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 116.6072° |
| argument of perigee: | 234.9595° |
| revolutions per day: | 14.90736305 |
| mean anomaly at epoch: | 125.1039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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