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 14700U 26087.98150551 +.00000000 +00000-0 +60472-4 0 00005
2 14700 82.5374 37.9623 0018705 180.8136 285.1485 14.85612964 00
| Epoch (UTC): | 28 March 2026 23:33:22 |
| Eccentricity: | 0.0018705 |
| inclination: | 82.5374° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 37.9623° |
| argument of perigee: | 180.8136° |
| revolutions per day: | 14.85612964 |
| mean anomaly at epoch: | 285.1485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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