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 36828U 26141.01113589 +.00000000 +00000-0 +00000-0 0 00002
2 36828 54.2967 163.2045 0058933 224.9850 321.8842 1.00280030 03
| Epoch (UTC): | 21 May 2026 00:16:02 |
| Eccentricity: | 0.0058933 |
| inclination: | 54.2967° |
| perigee height: | 35536 km |
| apogee height: | 36033 km |
| right ascension of ascending node: | 163.2045° |
| argument of perigee: | 224.9850° |
| revolutions per day: | 1.00280030 |
| mean anomaly at epoch: | 321.8842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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