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 26032.37360448 +.00000000 +00000-0 +30133-3 0 00003
2 39151 98.0988 172.2911 0011954 249.9599 110.0332 14.92781264 07
| Epoch (UTC): | 01 February 2026 08:57:59 |
| Eccentricity: | 0.0011954 |
| inclination: | 98.0988° |
| perigee height: | 581 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 172.2911° |
| argument of perigee: | 249.9599° |
| revolutions per day: | 14.92781264 |
| mean anomaly at epoch: | 110.0332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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