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 27940U 26020.20791208 +.00000000 +00000-0 +17563-3 0 00009
2 27940 98.3747 194.3107 0014148 102.3235 257.9554 14.69268516 06
| Epoch (UTC): | 20 January 2026 04:59:23 |
| Eccentricity: | 0.0014148 |
| inclination: | 98.3747° |
| perigee height: | 653 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 194.3107° |
| argument of perigee: | 102.3235° |
| revolutions per day: | 14.69268516 |
| mean anomaly at epoch: | 257.9554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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