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 26158.93178332 +.00000000 +00000-0 +22994-3 0 00007
2 18152 82.4858 316.0262 0009949 60.4320 299.7911 15.31734104 07
| Epoch (UTC): | 07 June 2026 22:21:46 |
| Eccentricity: | 0.0009949 |
| inclination: | 82.4858° |
| perigee height: | 464 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 316.0262° |
| argument of perigee: | 60.4320° |
| revolutions per day: | 15.31734104 |
| mean anomaly at epoch: | 299.7911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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