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 59481U 26088.07921176 +.00000000 +00000-0 +53769-4 0 00001
2 59481 98.7199 97.1033 0004638 180.7956 179.3214 14.20722046 07
| Epoch (UTC): | 29 March 2026 01:54:03 |
| Eccentricity: | 0.0004638 |
| inclination: | 98.7199° |
| perigee height: | 820 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 97.1033° |
| argument of perigee: | 180.7956° |
| revolutions per day: | 14.20722046 |
| mean anomaly at epoch: | 179.3214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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