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 18691U 26101.47301337 +.00000000 +00000-0 +11351-2 0 00009
2 18691 90.2293 355.3865 0024396 285.9823 198.8761 12.96735822 03
| Epoch (UTC): | 11 April 2026 11:21:08 |
| Eccentricity: | 0.0024396 |
| inclination: | 90.2293° |
| perigee height: | 1256 km |
| apogee height: | 1294 km |
| right ascension of ascending node: | 355.3865° |
| argument of perigee: | 285.9823° |
| revolutions per day: | 12.96735822 |
| mean anomaly at epoch: | 198.8761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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