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 39153U 26154.26760301 +.00000000 +00000-0 +38511-3 0 00008
2 39153 98.1668 313.5902 0011334 185.6911 174.4183 14.97215022 08
| Epoch (UTC): | 03 June 2026 06:25:20 |
| Eccentricity: | 0.0011334 |
| inclination: | 98.1668° |
| perigee height: | 568 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 313.5902° |
| argument of perigee: | 185.6911° |
| revolutions per day: | 14.97215022 |
| mean anomaly at epoch: | 174.4183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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