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 26071.15753353 +.00000000 +00000-0 +17360-3 0 00002
2 14781 97.7946 37.8942 0008579 136.5782 223.6113 14.90516363 05
| Epoch (UTC): | 12 March 2026 03:46:50 |
| Eccentricity: | 0.0008579 |
| inclination: | 97.7946° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 37.8942° |
| argument of perigee: | 136.5782° |
| revolutions per day: | 14.90516363 |
| mean anomaly at epoch: | 223.6113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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