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 18152U 26109.14206286 +.00000000 +00000-0 +18014-3 0 00004
2 18152 82.4890 6.4904 0007436 223.1097 136.9563 15.31141248 00
| Epoch (UTC): | 19 April 2026 03:24:34 |
| Eccentricity: | 0.0007436 |
| inclination: | 82.4890° |
| perigee height: | 467 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 6.4904° |
| argument of perigee: | 223.1097° |
| revolutions per day: | 15.31141248 |
| mean anomaly at epoch: | 136.9563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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