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 26061U 26155.21227836 +.00000000 +00000-0 +19674-3 0 00008
2 26061 100.2230 157.7485 0030900 267.0305 92.7343 14.45092904 03
| Epoch (UTC): | 04 June 2026 05:05:40 |
| Eccentricity: | 0.0030900 |
| inclination: | 100.2230° |
| perigee height: | 720 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 157.7485° |
| argument of perigee: | 267.0305° |
| revolutions per day: | 14.45092904 |
| mean anomaly at epoch: | 92.7343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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