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 15945U 26088.19970558 +.00000000 +00000-0 +66745-4 0 00007
2 15945 82.5305 6.5924 0020045 124.9836 235.3266 14.86454499 00
| Epoch (UTC): | 29 March 2026 04:47:34 |
| Eccentricity: | 0.0020045 |
| inclination: | 82.5305° |
| perigee height: | 595 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 6.5924° |
| argument of perigee: | 124.9836° |
| revolutions per day: | 14.86454499 |
| mean anomaly at epoch: | 235.3266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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