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 13819U 26159.53282755 +.00000000 +00000-0 +27798-3 0 00001
2 13819 81.1020 250.6212 0015904 91.3916 268.9152 15.49007142 08
| Epoch (UTC): | 08 June 2026 12:47:16 |
| Eccentricity: | 0.0015904 |
| inclination: | 81.1020° |
| perigee height: | 409 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 250.6212° |
| argument of perigee: | 91.3916° |
| revolutions per day: | 15.49007142 |
| mean anomaly at epoch: | 268.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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