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 13154U 26106.22470249 +.00000000 +00000-0 +54415-4 0 00005
2 13154 81.1518 172.6711 0027941 197.4659 162.5609 15.10278273 04
| Epoch (UTC): | 16 April 2026 05:23:34 |
| Eccentricity: | 0.0027941 |
| inclination: | 81.1518° |
| perigee height: | 516 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 172.6711° |
| argument of perigee: | 197.4659° |
| revolutions per day: | 15.10278273 |
| mean anomaly at epoch: | 162.5609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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