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 20437U 26106.64341042 +.00000000 +00000-0 +31876-4 0 00007
2 20437 98.8094 154.8643 0011517 85.6495 30.1772 14.33251829 07
| Epoch (UTC): | 16 April 2026 15:26:30 |
| Eccentricity: | 0.0011517 |
| inclination: | 98.8094° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 154.8643° |
| argument of perigee: | 85.6495° |
| revolutions per day: | 14.33251829 |
| mean anomaly at epoch: | 30.1772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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