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 59098U 26145.58340375 +.00000000 +00000-0 +24838-3 0 00005
2 59098 97.8489 277.2192 0012930 96.5245 263.7449 14.98416566 09
| Epoch (UTC): | 25 May 2026 14:00:06 |
| Eccentricity: | 0.0012930 |
| inclination: | 97.8489° |
| perigee height: | 563 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 277.2192° |
| argument of perigee: | 96.5245° |
| revolutions per day: | 14.98416566 |
| mean anomaly at epoch: | 263.7449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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