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 20798U 26087.89759972 +.00000000 +00000-0 +45468-3 0 00008
2 20798 98.7671 76.6592 0008360 172.8104 187.3195 14.22021145 07
| Epoch (UTC): | 28 March 2026 21:32:32 |
| Eccentricity: | 0.0008360 |
| inclination: | 98.7671° |
| perigee height: | 813 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 76.6592° |
| argument of perigee: | 172.8104° |
| revolutions per day: | 14.22021145 |
| mean anomaly at epoch: | 187.3195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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