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 26072.90296983 +.00000000 +00000-0 +18970-3 0 00005
2 14781 97.7952 39.6166 0008683 131.2522 228.9445 14.90522952 07
| Epoch (UTC): | 13 March 2026 21:40:16 |
| Eccentricity: | 0.0008683 |
| inclination: | 97.7952° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 39.6166° |
| argument of perigee: | 131.2522° |
| revolutions per day: | 14.90522952 |
| mean anomaly at epoch: | 228.9445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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