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 41783U 26098.26988586 +.00000000 +00000-0 +15361-3 0 00002
2 41783 97.8328 98.2069 0032782 81.8109 278.6812 14.67098207 03
| Epoch (UTC): | 08 April 2026 06:28:38 |
| Eccentricity: | 0.0032782 |
| inclination: | 97.8328° |
| perigee height: | 647 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 98.2069° |
| argument of perigee: | 81.8109° |
| revolutions per day: | 14.67098207 |
| mean anomaly at epoch: | 278.6812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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