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 18467U 26086.52742230 +.00000000 +00000-0 +16564-3 0 00001
2 18467 98.8302 111.1198 0091427 277.4085 238.6468 14.25756738 01
| Epoch (UTC): | 27 March 2026 12:39:29 |
| Eccentricity: | 0.0091427 |
| inclination: | 98.8302° |
| perigee height: | 740 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 111.1198° |
| argument of perigee: | 277.4085° |
| revolutions per day: | 14.25756738 |
| mean anomaly at epoch: | 238.6468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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