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 26545U 26087.96834690 +.00000000 +00000-0 +17302-3 0 00009
2 26545 64.5516 189.5816 0037954 312.3343 47.4554 14.92946097 06
| Epoch (UTC): | 28 March 2026 23:14:25 |
| Eccentricity: | 0.0037954 |
| inclination: | 64.5516° |
| perigee height: | 562 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 189.5816° |
| argument of perigee: | 312.3343° |
| revolutions per day: | 14.92946097 |
| mean anomaly at epoch: | 47.4554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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