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 26384U 26106.88258639 +.00000000 +00000-0 +80856-4 0 00001
2 26384 97.8380 84.3921 0012901 183.1788 176.9340 14.71265235 02
| Epoch (UTC): | 16 April 2026 21:10:55 |
| Eccentricity: | 0.0012901 |
| inclination: | 97.8380° |
| perigee height: | 648 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 84.3921° |
| argument of perigee: | 183.1788° |
| revolutions per day: | 14.71265235 |
| mean anomaly at epoch: | 176.9340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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