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 39151U 26144.34888438 +.00000000 +00000-0 +22047-3 0 00003
2 39151 98.1194 287.7180 0011473 239.1251 120.8840 14.93521589 05
| Epoch (UTC): | 24 May 2026 08:22:23 |
| Eccentricity: | 0.0011473 |
| inclination: | 98.1194° |
| perigee height: | 579 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 287.7180° |
| argument of perigee: | 239.1251° |
| revolutions per day: | 14.93521589 |
| mean anomaly at epoch: | 120.8840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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