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 36101U 26145.59378182 +.00000000 +00000-0 +00000-0 0 00005
2 36101 0.4362 80.7844 0005801 339.6444 87.0045 1.00270476 07
| Epoch (UTC): | 25 May 2026 14:15:02 |
| Eccentricity: | 0.0005801 |
| inclination: | 0.4362° |
| perigee height: | 35763 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 80.7844° |
| argument of perigee: | 339.6444° |
| revolutions per day: | 1.00270476 |
| mean anomaly at epoch: | 87.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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