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 26020.69519376 +.00000000 +00000-0 +91759-4 0 00006
2 14700 82.5361 101.0905 0020023 51.4042 64.8429 14.85537746 01
| Epoch (UTC): | 20 January 2026 16:41:04 |
| Eccentricity: | 0.0020023 |
| inclination: | 82.5361° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 101.0905° |
| argument of perigee: | 51.4042° |
| revolutions per day: | 14.85537746 |
| mean anomaly at epoch: | 64.8429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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